METRIC

MIL-STD-461F
10 December 2007
___________________________

SUPERSEDING
MIL-STD-461E
20 August 1999

DEPARTMENT OF DEFENSE
INTERFACE STANDARD
REQUIREMENTS FOR THE CONTROL OF
ELECTROMAGNETIC INTERFERENCE
CHARACTERISTICS OF SUBSYSTEMS AND
EQUIPMENT

AMSC 9034 AREA EMCS

DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited.

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 MIL-STD-461F

FOREWORD

1. This standard is approved for use by all Departments and Agencies of the Department of
Defense.

2. Comments, suggestions, or questions on this document should be addressed to

ASC/ENOI, 2530 Loop Road W, Wright-Patterson AFB OH 45433-7101, or emailed to
Engineering.Standards@wpafb.af.mil. Since contact information can change, you may want to
verify the currency of this address information using the ASSIST Online database at
http://assist.daps.dla.mil/.

3. The stated interface requirements are considered necessary to provide reasonable confidence
that a particular subsystem or equipment complying with these requirements will function within
their designated design tolerances when operating in their intended electromagnetic environment
(EME). The procuring activity should consider tailoring the individual requirements to be more
or less severe based on the design features of the intended platform and its mission in concert
with personnel knowledgeable about electromagnetic compatibility (EMC) issues affecting
platform integration.

4. An appendix is included which provides the rationale and background for each requirement
and verification section.

5. A committee consisting of representatives of the Army, Air Force, Navy, other DoD agencies,
and industry prepared this document.

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 MIL-STD-461F

CONTENTS

PARAGRAPH PAGE

1. SCOPE ...................................................................................................................................... 1
1.1 Purpose. ............................................................................................................................ 1
1.2 Application. ...................................................................................................................... 1
1.2.1 General applicability. ............................................................................................. 1
1.2.2 Tailoring of requirements. ...................................................................................... 1
1.3 Structure............................................................................................................................ 1
1.4 Emission and susceptibility designations. ........................................................................ 1
2. APPLICABLE DOCUMENTS............................................................................................... 3
2.1 General.............................................................................................................................. 3
2.2 Government documents. ................................................................................................... 3
2.2.1 Government documents, drawings, and publications............................................. 3
2.3 Non-Government publications.......................................................................................... 3
2.4 Order of precedence.......................................................................................................... 4
3. DEFINITIONS ......................................................................................................................... 5
3.1 General.............................................................................................................................. 5
3.2 Acronyms used in this standard........................................................................................ 5
3.3 Above deck. ...................................................................................................................... 5
3.4 Below deck. ...................................................................................................................... 5
3.5 External installation.......................................................................................................... 6
3.6 Flight-line equipment. ...................................................................................................... 6
3.7 Internal installation. .......................................................................................................... 6
3.8 Metric units....................................................................................................................... 6
3.9 Non-developmental item (NDI)........................................................................................ 6
3.10 Safety critical. ................................................................................................................. 6
3.11 Test setup boundary........................................................................................................ 6
4. GENERAL REQUIREMENTS .............................................................................................. 7
4.1 General.............................................................................................................................. 7
4.2 Interface requirements. ..................................................................................................... 7
4.2.1 Joint procurement. .................................................................................................. 7
4.2.2 Filtering (Navy only).............................................................................................. 7
4.2.3 Self-compatibility. .................................................................................................. 7
4.2.4 Non-developmental items (NDI)............................................................................ 7
4.2.4.1 Commercial items (CI). ....................................................................................... 7
4.2.4.1.1 Selected by contractor...............................................................................................7
4.2.4.1.2 Specified by procuring activity. ...............................................................................7
4.2.4.2 Procurement of equipment or subsystems having met other EMI
requirements. ................................................................................................. 8
4.2.5 Government furnished equipment (GFE). .............................................................. 8
4.2.6 Switching transients. .............................................................................................. 8
4.2.7 Interchangeable modular equipment ...................................................................... 8
4.3 Verification requirements. ................................................................................................ 8

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4.3.1 Measurement tolerances. ........................................................................................ 8
4.3.2 Shielded enclosures. ............................................................................................... 9
4.3.2.1 Radio Frequency (RF) absorber material. ........................................................... 9
4.3.3 Other test sites. ....................................................................................................... 9
4.3.4 Ambient electromagnetic level............................................................................... 9
4.3.5 Ground plane. ....................................................................................................... 10
4.3.5.1 Metallic ground plane........................................................................................ 10
4.3.5.2 Composite ground plane.................................................................................... 10
4.3.6 Power source impedance. ..................................................................................... 10
4.3.7 General test precautions. ...................................................................................... 10
4.3.7.1 Accessory equipment......................................................................................... 10
4.3.7.2 Excess personnel and equipment....................................................................... 10
4.3.7.3 Overload precautions......................................................................................... 11
4.3.7.4 RF hazards. ........................................................................................................ 11
4.3.7.5 Shock hazard. .................................................................................................... 11
4.3.7.6 Federal Communications Commission (FCC) restrictions................................ 11
4.3.8 EUT test configurations........................................................................................ 11
4.3.8.1 EUT design status.............................................................................................. 11
4.3.8.2 Bonding of EUT. ............................................................................................... 11
4.3.8.3 Shock and vibration isolators. ........................................................................... 11
4.3.8.4 Safety grounds. .................................................................................................. 11
4.3.8.5 Orientation of EUTs. ......................................................................................... 11
4.3.8.6 Construction and arrangement of EUT cables................................................... 12
4.3.8.6.1 Interconnecting leads and cables............................................................................12
4.3.8.6.2 Input (primary) power leads. ..................................................................................12
4.3.8.7 Electrical and mechanical interfaces. ................................................................ 12
4.3.9 Operation of EUT. ................................................................................................ 13
4.3.9.1 Operating frequencies for tunable RF equipment. ............................................ 13
4.3.9.2 Operating frequencies for spread spectrum equipment. .................................... 13
4.3.9.3 Susceptibility monitoring. ................................................................................. 13
4.3.10 Use of measurement equipment. ........................................................................ 13
4.3.10.1 Detector. .......................................................................................................... 13
4.3.10.2 Computer-controlled instrumentation. ............................................................ 14
4.3.10.3 Emission testing............................................................................................... 14
4.3.10.3.1 Bandwidths............................................................................................................14
4.3.10.3.2 Emission identification. ........................................................................................14
4.3.10.3.3 Frequency scanning. .............................................................................................14
4.3.10.3.4 Emission data presentation. ..................................................................................15
4.3.10.4 Susceptibility testing. ...................................................................................... 15
4.3.10.4.1 Frequency scanning. .............................................................................................15
4.3.10.4.2 Modulation of susceptibility signals. ...................................................................15
4.3.10.4.3 Thresholds of susceptibility..................................................................................15
4.3.11 Calibration of measuring equipment. ................................................................. 16

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4.3.11.1 Measurement system test................................................................................. 16
4.3.11.2 Antenna factors................................................................................................ 16
5. DETAILED REQUIREMENTS........................................................................................... 24
5.1 General............................................................................................................................ 24
5.1.1 Units of frequency domain measurements. .......................................................... 24
5.2 EMI control requirements versus intended installations. ............................................... 24
5.3 Emission and susceptibility requirements, limits, and test procedures. ......................... 24
5.4 CE101, conducted emissions, power leads, 30 Hz to 10 kHz. ....................................... 27
5.4.1 CE101 applicability. ............................................................................................. 27
5.4.2 CE101 limits......................................................................................................... 27
5.4.3 CE101 test procedure. .......................................................................................... 27
5.4.3.1 Purpose. ............................................................................................................. 27
5.4.3.2 Test equipment. ................................................................................................. 27
5.4.3.3 Setup. ................................................................................................................. 27
5.4.3.4 Procedures. ........................................................................................................ 28
5.4.3.5 Data presentation. .............................................................................................. 28
5.5 CE102, conducted emissions, power leads, 10 kHz to 10 MHz..................................... 35
5.5.1 CE102 applicability. ............................................................................................. 35
5.5.2 CE102 limits......................................................................................................... 35
5.5.3 CE102 test procedure. .......................................................................................... 35
5.5.3.1 Purpose. ............................................................................................................. 35
5.5.3.2 Test equipment. ................................................................................................. 35
5.5.3.3 Setup. ................................................................................................................. 35
5.5.3.4 Procedures. ........................................................................................................ 35
5.5.3.5 Data presentation. .............................................................................................. 36
5.6 CE106, conducted emissions, antenna terminal, 10 kHz to 40 GHz.............................. 40
5.6.1 CE106 applicability. ............................................................................................. 40
5.6.2 CE106 limits......................................................................................................... 40
5.6.3 CE106 test procedure. .......................................................................................... 40
5.6.3.1 Purpose. ............................................................................................................. 40
5.6.3.2 Test equipment. ................................................................................................. 40
5.6.3.3 Setup. ................................................................................................................. 41
5.6.3.4 Procedures. ........................................................................................................ 41
5.6.3.4.1 Transmit mode for transmitters and amplifiers......................................................41
5.6.3.4.2 Receivers and stand-by mode for transmitters and amplifiers. .............................42
5.6.3.5 Data presentation. .............................................................................................. 43
5.6.3.5.1 Transmit mode for transmitters and amplifiers......................................................43
5.6.3.5.2 Receivers and stand-by mode for transmitters and amplifiers. .............................43
5.7 CS101, conducted susceptibility, power leads, 30 Hz to 150 kHz................................. 47
5.7.1 CS101 applicability. ............................................................................................. 47
5.7.2 CS101 limit........................................................................................................... 47
5.7.3 CS101 test procedure............................................................................................ 47

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5.7.3.1 Purpose. ............................................................................................................. 47
5.7.3.2 Test equipment. ................................................................................................. 47
5.7.3.3 Setup. ................................................................................................................. 47
5.7.3.4 Procedures. ........................................................................................................ 48
5.7.3.5 Data presentation. .............................................................................................. 49
5.8 CS103, conducted susceptibility, antenna port, intermodulation, 15 kHz to 10
GHz..................................................................................................................... 56
5.8.1 CS103 applicability. ............................................................................................. 56
5.8.2 CS103 limit........................................................................................................... 56
5.8.3 CS103 test procedures. ......................................................................................... 56
5.8.3.1 Purpose. ............................................................................................................. 56
5.8.3.2 Test requirements. ............................................................................................. 56
5.9 CS104, conducted susceptibility, antenna port, rejection of undesired signals,
30 Hz to 20 GHz................................................................................................. 57
5.9.1 CS104 applicability. ............................................................................................. 57
5.9.2 CS104 limit........................................................................................................... 57
5.9.3 CS104 test procedures. ........................................................................................ 57
5.9.3.1 Purpose. ............................................................................................................. 57
5.9.3.2 Test requirements. ............................................................................................. 57
5.10 CS105, conducted susceptibility, antenna port, cross modulation, 30 Hz to
20 GHz................................................................................................................ 58
5.10.1 CS105 applicability. ........................................................................................... 58
5.10.2 CS105 limit......................................................................................................... 58
5.10.3 CS105 test procedures. ...................................................................................... 58
5.10.3.1 Purpose. ........................................................................................................... 58
5.10.3.2 Test requirements. ........................................................................................... 58
5.11 CS106, conducted susceptibility, transients, power leads. ........................................... 59
5.11.1 CS106 Applicability. .......................................................................................... 59
5.11.2 CS106 limit......................................................................................................... 59
5.11.3 CS106 test procedure.......................................................................................... 59
5.11.3.1 Purpose. ........................................................................................................... 59
5.11.3.2 Test equipment. ............................................................................................... 59
5.11.3.3 Setup. ............................................................................................................... 59
5.11.3.4 Procedures. ...................................................................................................... 59
5.11.3.5 Data presentation. ............................................................................................ 60
5.12 CS109, conducted susceptibility, structure current, 60 Hz to 100 kHz........................ 66
5.12.1 CS109 applicability. ........................................................................................... 66
5.12.2 CS109 limit......................................................................................................... 66
5.12.3 CS109 test procedures. ....................................................................................... 66
5.12.3.1 Purpose. ........................................................................................................... 66
5.12.3.2 Test equipment. ............................................................................................... 66
5.12.3.3 Setup. ............................................................................................................... 66
5.12.3.4 Procedures. ...................................................................................................... 67

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5.12.3.5 Data presentation. ............................................................................................ 67
5.13 CS114, conducted susceptibility, bulk cable injection, 10 kHz to 200 MHz. .............. 70
5.13.1 CS114 applicability. ........................................................................................... 70
5.13.2 CS114 limit......................................................................................................... 70
5.13.3 CS114 test procedures. ....................................................................................... 70
5.13.3.1 Purpose. ........................................................................................................... 70
5.13.3.2 Test equipment. ............................................................................................... 70
5.13.3.3 Setup. ............................................................................................................... 71
5.13.3.4 Procedures. ...................................................................................................... 71
5.13.3.5 Data presentation. ............................................................................................ 72
5.14 CS115, Conducted susceptibility, bulk cable injection, impulse excitation................. 78
5.14.1 CS115 applicability. ........................................................................................... 78
5.14.2 CS115 limit......................................................................................................... 78
5.14.3 CS115 test procedures. ....................................................................................... 78
5.14.3.1 Purpose. ........................................................................................................... 78
5.14.3.2 Test equipment. ............................................................................................... 78
5.14.3.3 Setup. ............................................................................................................... 78
5.14.3.4 Procedures. ...................................................................................................... 79
5.14.3.5 Data presentation. ............................................................................................ 80
5.15 CS116, conducted susceptibility, damped sinusoidal transients, cables and
power leads, 10 kHz to 100 MHz....................................................................... 84
5.15.1 CS116 applicability. ........................................................................................... 84
5.15.2 CS116 limit......................................................................................................... 84
5.15.3 CS116 test procedures. ....................................................................................... 84
5.15.3.1 Purpose. ........................................................................................................... 84
5.15.3.2 Test equipment. ............................................................................................... 84
5.15.3.3 Setup. ............................................................................................................... 84
5.15.3.4 Procedures. ...................................................................................................... 85
5.15.3.5 Data presentation. ............................................................................................ 86
5.16 RE101, radiated emissions, magnetic field, 30 Hz to 100 kHz. ................................... 91
5.16.1 RE101 applicability. ........................................................................................... 91
5.16.2 RE101 limit. ....................................................................................................... 91
5.16.3 RE101 test procedures........................................................................................ 91
5.16.3.1 Purpose. ........................................................................................................... 91
5.16.3.2 Test equipment. ............................................................................................... 91
5.16.3.3 Setup. ............................................................................................................... 91
5.16.3.4 Procedures. ...................................................................................................... 91
5.16.3.5 Data presentation. ............................................................................................ 93
5.17 RE102, radiated emissions, electric field, 10 kHz to 18 GHz. ..................................... 98
5.17.1 RE102 applicability. ........................................................................................... 98
5.17.2 RE102 limits....................................................................................................... 98
5.17.3 RE102 test procedures........................................................................................ 98
5.17.3.1 Purpose. ........................................................................................................... 98

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5.17.3.2 Test equipment. ............................................................................................... 98
5.17.3.3 Setup. ............................................................................................................... 99
5.17.3.4 Procedures. .................................................................................................... 100
5.17.3.5 Data presentation. .......................................................................................... 101
5.18 RE103, radiated emissions, antenna spurious and harmonic outputs, 10 kHz
to 40 GHz. ........................................................................................................ 110
5.18.1 RE103 applicability. ......................................................................................... 110
5.18.2 RE103 limits..................................................................................................... 110
5.18.3 RE103 test procedures...................................................................................... 110
5.18.3.1 Purpose. ......................................................................................................... 110
5.18.3.2 Test equipment. ............................................................................................. 110
5.18.3.3 Setup. ............................................................................................................. 110
5.18.3.4 Procedures. .................................................................................................... 111
5.18.3.5 Data presentation. .......................................................................................... 113
5.19 RS101, radiated susceptibility, magnetic field, 30 Hz to 100 kHz............................. 116
5.19.1 RS101 applicability. ......................................................................................... 116
5.19.2 RS101 limit....................................................................................................... 116
5.19.3 RS101 test procedures. ..................................................................................... 116
5.19.3.1 Purpose. ......................................................................................................... 116
5.19.3.2 Test equipment. ............................................................................................. 116
5.19.3.3 Setup. ............................................................................................................. 117
5.19.3.4 Procedures. .................................................................................................... 117
5.19.3.5 Data presentation. .......................................................................................... 118
5.19.4 RS101 alternative test procedures – AC Helmholtz coil.................................. 118
5.19.4.1 Purpose. ......................................................................................................... 118
5.19.4.2 Test equipment. ............................................................................................. 118
5.19.4.3 Setup. ............................................................................................................. 118
5.19.4.4 Procedures. .................................................................................................... 119
5.19.4.5 Data presentation. .......................................................................................... 120
5.20 RS103, radiated susceptibility, electric field, 2 MHz to 40 GHz. .............................. 127
5.20.1 RS103 applicability. ......................................................................................... 127
5.20.2 RS103 limit....................................................................................................... 127
5.20.3 RS103 test procedures. ..................................................................................... 127
5.20.3.1 Purpose. ......................................................................................................... 127
5.20.3.2 Test equipment. ............................................................................................. 127
5.20.3.3 Setup. ............................................................................................................. 128
5.20.3.4 Procedures. .................................................................................................... 129
5.20.3.5 Data presentation. .......................................................................................... 130
5.20.4 RS103 alternative test procedures – reverberation chamber (mode-
tuned)......................................................................................................... 131
5.20.4.1 Purpose. ......................................................................................................... 131
5.20.4.2 Test equipment. ............................................................................................. 131
5.20.4.3 Setup. ............................................................................................................. 131

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5.20.4.4 Procedure....................................................................................................... 132
5.20.4.5 Data presentation. .......................................................................................... 133
5.21 RS105, radiated susceptibility, transient electromagnetic field. ................................ 143
5.21.1 RS105 applicability. ......................................................................................... 143
5.21.2 RS105 limit....................................................................................................... 143
5.21.3 RS105 test procedures. ..................................................................................... 143
5.21.3.1 Purpose. ......................................................................................................... 143
5.21.3.2 Test equipment. ............................................................................................. 143
5.20.3.3 Setup. ............................................................................................................. 143
5.21.3.4 Procedures. .................................................................................................... 144
5.21.3.5 Data presentation. .......................................................................................... 145
6. NOTES .................................................................................................................................. 149
6.1 Intended use. ................................................................................................................. 149
6.2 Acquisition requirements.............................................................................................. 149
6.3 Associated Data Item Descriptions (DIDs). ................................................................. 149
6.4 Tailoring guidance. ....................................................................................................... 149
6.5 Subject term (key word) listing. ................................................................................... 149
6.6 International standardization agreement implementation............................................. 150
6.7 Changes from previous issue. ....................................................................................... 150
6.8 Technical points of contact........................................................................................... 150

APPENDIX

APPENDIX A APPLICATION GUIDE .................................................................................151

A.1 GENERAL......................................................................................................................... 151
A.1.1 Scope......................................................................................................................... 151
A.1.2 Structure.................................................................................................................... 151
A.2 APPLICABLE DOCUMENTS ........................................................................................ 152
A.2.1 General...................................................................................................................... 152
A.2.2 Government documents. ........................................................................................... 152
A.2.2.1 Specifications, standards, and handbooks. ..................................................... 152
A.2.2.2 Other Government documents, drawings, and publications........................... 153
A.2.3 Non-Government publications.................................................................................. 154
A.3 DEFINITIONS .................................................................................................................. 157
A.3.1 General...................................................................................................................... 157
A.3.2 Acronyms used in this appendix............................................................................... 157
A.3.3 Below deck. .............................................................................................................. 158
A.3.4 External installation. ................................................................................................. 158
A.3.5 Internal installation. .................................................................................................. 158
A.3.6 Metric units. .............................................................................................................. 158

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A.3.7 Non-developmental item........................................................................................... 158
A.3.8 Safety critical. ........................................................................................................... 158
A.3.9 Test setup boundary. ................................................................................................. 158
A.4 GENERAL REQUIREMENTS ....................................................................................... 159
A.4.1 (4.1) General. ............................................................................................................ 159
A.4.2 (4.2) Interface Requirements. ................................................................................... 160
A.4.2.1 (4.2.1) Joint procurement................................................................................ 160
A.4.2.2 (4.2.2) Filtering (Navy only). ......................................................................... 160
A.4.2.3 (4.2.3) Self-compatibility. .............................................................................. 160
A.4.2.4 (4.2.4) Non-Developmental Items (NDI). ...................................................... 161
A.4.2.4.1 (4.2.4.1) Commercial items (CI). ................................................................ 162
A.4.2.4.1.1 (4.2.4.1.1) Selected by contractor.....................................................................163
A.4.2.4.1.2 (4.2.4.1.2) Specified by procuring activity. .....................................................163
A.4.2.4.2. (4.2.4.2) Procurement of equipment or subsystems having met other
EMI requirements. ............................................................................................164
A.4.2.5 (4.2.5) Government Furnished Equipment (GFE).......................................... 164
A.4.2.6 (4.2.6) Switching transients. ........................................................................... 164
A.4.2.7 (4.2.7) Interchangeable modular equipment................................................... 165
A.4.3 (4.3) Verification requirements. ............................................................................... 166
A.4.3.1 (4.3.1) Measurement tolerances...................................................................... 169
A.4.3.2 (4.3.2) Shielded enclosures............................................................................. 169
A.4.3.2.1 (4.3.2.1) Radio Frequency (RF) absorber material...................................... 170
A.4.3.3 (4.3.3) Other test sites..................................................................................... 170
A.4.3.4 (4.3.4) Ambient electromagnetic level. .......................................................... 171
A.4.3.5 (4.3.5) Ground plane....................................................................................... 171
A.4.3.5.1 (4.3.5.1) Metallic ground plane. .................................................................. 172
A.4.3.5.2 (4.3.5.2) Composite ground plane. .............................................................. 173
A.4.3.6 (4.3.6) Power source impedance..................................................................... 173
A.4.3.7 (4.3.7) General test precautions...................................................................... 176
A.4.3.7.1 (4.3.7.1) Accessory equipment. ................................................................... 176
A.4.3.7.2 (4.3.7.2) Excess personnel and equipment. ................................................. 177
A.4.3.7.3 (4.3.7.3) Overload precautions. ................................................................... 177
A.4.3.7.4 (4.3.7.4) RF hazards. ................................................................................... 178
A.4.3.7.5 (4.3.7.5) Shock hazard................................................................................. 178
A.4.3.7.6 (4.3.7.6) Federal Communications Commission (FCC) restrictions. .......... 178
A.4.3.8 (4.3.8) EUT test configurations. ..................................................................... 179
A.4.3.8.1 (4.3.8.1) EUT design status. ........................................................................ 179
A.4.3.8.2 (4.3.8.2) Bonding of EUT............................................................................ 179
A.4.3.8.3 (4.3.8.3) Shock and vibration isolators........................................................ 179
A.4.3.8.4 (4.3.8.4) Safety grounds. ............................................................................. 180
A.4.3.8.5 (4.3.8.5) Orientation of EUTs...................................................................... 180
A.4.3.8.6 (4.3.8.6) Construction and arrangement of EUT cables. ............................. 180

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A.4.3.8.6.1 (4.3.8.6.1) Interconnecting leads and cables....................................................181
A.4.3.8.6.2 (4.3.8.6.2) Input (primary) power leads. ..........................................................182
A.4.3.8.7 (4.3.8.7) Electrical and mechanical interfaces............................................. 183
A.4.3.9 (4.3.9) Operation of EUT. .............................................................................. 184
A.4.3.9.1 (4.3.9.1) Operating frequencies for tunable RF equipment......................... 184
A.4.3.9.2 (4.3.9.2) Operating frequencies for spread spectrum equipment. ............... 185
A.4.3.9.3 (4.3.9.3) Susceptibility monitoring.............................................................. 186
A.4.3.10 (4.3.10) Use of measurement equipment...................................................... 186
A.4.3.10.1 (4.3.10.1) Detector..................................................................................... 187
A.4.3.10.2 (4.3.10.2) Computer-controlled instrumentation....................................... 189
A.4.3.10.3 (4.3.10.3) Emission testing. ....................................................................... 189
A.4.3.10.3.1 (4.3.10.3.1) Bandwidths. ................................................................................189
A.4.3.10.3.2 (4.3.10.3.2) Emission identification. ..............................................................192
A.4.3.10.3.3 (4.3.10.3.3) Frequency scanning. ...................................................................192
A.4.3.10.3.4 (4.3.10.3.4) Emission data presentation.........................................................193
A.4.3.10.4 (4.3.10.4) Susceptibility testing................................................................. 195
A.4.3.10.4.1 (4.3.10.4.1) Frequency scanning. ...................................................................195
A.4.3.10.4.2 (4.3.10.4.2) Modulation of susceptibility signals. .........................................197
A.4.3.10.4.3 (4.3.10.4.3) Thresholds of susceptibility........................................................199
A.4.3.11 (4.3.11) Calibration of measuring equipment............................................... 199
A.4.3.11.1 (4.3.11.1) Measurement system test. ......................................................... 200
A.4.3.11.2 (4.3.11.2) Antenna factors. ........................................................................ 200
A.5. DETAILED REQUIREMENTS ..................................................................................... 201
A.5.1 (5.1) General. ............................................................................................................ 201
A.5.1.1 (5.1.1) Units of frequency domain measurements.......................................... 203
A.5.2 (5.2) EMI control requirements versus intended installations.................................. 203
A.5.3 (5.3) Emission and susceptibility requirements, limits, and test procedures............ 204
A.5.4 (5.4) CE101, conducted emissions, power leads, 30 Hz to 10 kHz. ........................204
A.5.5 (5.5) CE102, conducted emissions, power leads, 10 kHz to 10 MHz. ..................... 207
A.5.6 (5.6) CE106, conducted emissions, antenna terminal, 10 kHz to 40 GHz. .............. 211
A.5.7 (5.7) CS101, conducted susceptibility, power leads, 30 Hz to 150 kHz. ................. 213
A.5.8 (5.8) CS103, conducted susceptibility, antenna port, intermodulation, 15
kHz to 10 GHz.................................................................................................. 215
A.5.9 (5.9) CS104, conducted susceptibility, antenna port, rejection of undesired
signals, 30 Hz to 20 GHz.................................................................................. 218
A.5.10 (5.10) CS105, conducted susceptibility, antenna port, cross modulation,
30 Hz to 20 GHz............................................................................................... 221
A.5.11 (5.11) CS106, conducted susceptibility, transients, power leads. .......................... 223
A.5.12 (5.12) CS109, conducted susceptibility, structure current, 60 Hz to 100
kHz. .................................................................................................................. 225
A.5.13 (5.13) CS114, conducted susceptibility, bulk cable injection, 10 kHz to
400 MHz........................................................................................................... 226

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CONTENTS

PARAGRAPH PAGE
A.5.14 (5.14) CS115, conducted susceptibility, bulk cable injection, impulse
excitation. ......................................................................................................... 232
A.5.15 (5.15) CS116, conducted susceptibility, damped sinusoid transients,
cables and power leads, 10 kHz to 100 MHz. .................................................. 235
A.5.16 (5.16) RE101, radiated emissions, magnetic field, 30 Hz to 100 kHz.................... 237
A.5.17 (5.17) RE102, radiated emissions, electric field, 10 kHz to 18 GHz. .................... 238
A.5.18 (5.18) RE103, radiated emissions, antenna spurious and harmonic
outputs, 10 kHz to 40 GHz. .............................................................................. 243
A.5.19 (5.19) RS101, radiated susceptibility, magnetic fields, 30 Hz to 100 kHz............. 244
A.5.20 (5.20) RS103, radiated susceptibility, electric field, 10 kHz to 40 GHz. ............... 247
A.5.21 (5.21) RS105, radiated susceptibility, transient, electromagnetic field.................. 253

FIGURE
FIGURE 1. RF absorber loading diagram. .................................................................................. 17
FIGURE 2. General test setup. .................................................................................................... 18
FIGURE 3. Test setup for non-conductive surface mounted EUT.............................................. 19
FIGURE 4. Test setup for free standing EUT in shielded enclosure........................................... 20
FIGURE 5. Test setup for free standing EUT.............................................................................. 21
FIGURE 6. LISN schematic. ....................................................................................................... 22
FIGURE 7. LISN impedance....................................................................................................... 23
FIGURE CE101-1. CE101 limit for submarine applications, DC............................................... 29
FIGURE CE101-2. CE101 limit for surface ships and submarine applications, 60 Hz. ............. 30
FIGURE CE101-3. CE101 limit for surface ships and submarine applications, 400
Hz.............................................................................................................. 31
FIGURE CE101-4. CE101 limit for Navy ASW aircraft and Army aircraft (including
flight line) applications. ............................................................................ 32
FIGURE CE101-5. Measurement system check. ........................................................................ 33
FIGURE CE101-6. Measurement setup. ..................................................................................... 34
FIGURE CE102-1. CE102 limit (EUT power leads, AC and DC) for all applications. ............. 37
FIGURE CE102-2. Measurement system check setup. ............................................................... 38
FIGURE CE102-3. Measurement setup. ..................................................................................... 39
FIGURE CE106-1. Setup for low power transmitters and amplifiers. ........................................ 44
FIGURE CE106-2. Setup for high power transmitters and amplifiers........................................ 45
FIGURE CE106-3. Setup for receivers and stand-by mode for transmitters and
amplifiers. ................................................................................................. 46
FIGURE CS101-1. CS101 voltage limit for all applications....................................................... 50
FIGURE CS101-2. CS101 power limit for all applications. ....................................................... 51
FIGURE CS101-3. Calibration.................................................................................................... 52
FIGURE CS101-4. Signal injection, DC or single phase AC. .................................................... 53
FIGURE CS101-5. Signal injection, 3-phase ungrounded. ......................................................... 54
FIGURE CS101-6. Signal injection, 3-phase wye. ..................................................................... 55

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CONTENTS

FIGURE PAGE
FIGURE CS106-1. CS106 voltage limit...................................................................................... 61
FIGURE CS106-2. Calibration.................................................................................................... 62
FIGURE CS106-3. Signal injection, DC or single phase AC. .................................................... 63
FIGURE CS106-4. Signal injection, 3-phase ungrounded. ......................................................... 64
FIGURE CS106-5. Signal injection, 3-phase wye. ..................................................................... 65
FIGURE CS109-1. CS109 limit. ................................................................................................. 68
FIGURE CS109-2. Test configuration. ....................................................................................... 69
FIGURE CS114-1. CS114 calibration limits............................................................................... 74
FIGURE CS114-2. Maximum insertion loss for injection probes............................................... 75
FIGURE CS114-3. Calibration setup. ......................................................................................... 76
FIGURE CS114-4. Bulk cable injection evaluation.................................................................... 77
FIGURE CS115-1. CS115 signal characteristics for all applications. ........................................ 81
FIGURE CS115-2. Calibration setup. ......................................................................................... 82
FIGURE CS115-3. Bulk cable injection...................................................................................... 83
FIGURE CS116-1. Typical CS116 damped sinusoidal waveform.............................................. 87
FIGURE CS116-2. CS116 limit for all applications. .................................................................. 88
FIGURE CS116-3. Typical test setup for calibration of test waveform...................................... 89
FIGURE CS116-4. Typical set up for bulk cable injection of damped sinusoidal
transients. .................................................................................................. 90
FIGURE RE101-1. RE101 limit for all Army applications......................................................... 94
FIGURE RE101-2. RE101 limit for all Navy applications. ........................................................ 95
FIGURE RE101-3. Calibration configuration. ............................................................................ 96
FIGURE RE101-4. Basic test setup............................................................................................. 97
FIGURE RE102-1. RE102 limit for surface ship applications.................................................. 102
FIGURE RE102-2. RE102 limit for submarine applications. ................................................... 103
FIGURE RE102-3. RE102 limit for aircraft and space system applications............................. 104
FIGURE RE102-4. RE102 limit for ground applications.......................................................... 105
FIGURE RE102-5. Basic test setup........................................................................................... 106
FIGURE RE102-6. Antenna positioning. .................................................................................. 107
FIGURE RE102-7. Multiple antenna positions......................................................................... 108
FIGURE RE102-8. Rod antenna system check. ........................................................................ 109
FIGURE RE103-1. Calibration and test setup for radiated harmonics and spurious
emissions, 10 kHz to 1 GHz. .................................................................. 114
FIGURE RE103-2. Calibration and test setup for radiated harmonics and spurious
emissions, 1 GHz to 40 GHz................................................................... 115
FIGURE RS101-1. RS101 limit for all Navy applications........................................................ 121
FIGURE RS101-2. RS101 limit for all Army applications. ...................................................... 122
FIGURE RS101-3. Calibration of the radiating system. ........................................................... 123
FIGURE RS101-4. Basic test setup. .......................................................................................... 124
FIGURE RS101-5. Calibration of Helmholtz coils. .................................................................. 125
FIGURE RS101-6. Test setup for Helmholtz coils. .................................................................. 126
FIGURE RS103-1. Test equipment configuration..................................................................... 137
FIGURE RS103-2. Multiple test antenna locations for frequency > 200 MHz. ....................... 138

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FIGURE PAGE
FIGURE RS103-3. Multiple test antenna locations for N positions, D > 3 meters................... 139
FIGURE RS103-4. Receive antenna procedure (1 to 40 GHz). ................................................ 140
FIGURE RS103-5. Reverberation chamber setup. .................................................................... 141
FIGURE RS103-6. Reverberation chamber overview............................................................... 142
FIGURE RS105-1. RS105 limit for all applications. ................................................................ 146
FIGURE RS105-2. Typical calibration setup using parallel plate radiation system. ................ 147
FIGURE RS105-3. Typical test setup using parallel plate radiation system............................. 148

FIGURE A-1. Voltage probe for tests at user’s installation. ..................................................... 168
FIGURE A-2. 5 μH LISN schematic. ........................................................................................ 175
FIGURE A-3. 5 μH LISN impedance........................................................................................ 175
FIGURE A-4. Peak detector response. ...................................................................................... 188
FIGURE A-5. Example of data presentation resolution. ........................................................... 194
FIGURE A-6. CE101 limits for a 5 μH LISN ........................................................................... 206
FIGURE A-7. Correction factor for 50 μH LISN coupling capacitor. ...................................... 210
FIGURE A-8. CS101 power amplifier protection. .................................................................... 215
FIGURE A-9. CS103 General test setup. .................................................................................. 217
FIGURE A-10. CS104 General test setup. ................................................................................ 220
FIGURE A-11. CS105 General test setup. ................................................................................ 223
FIGURE A-12. Typical CS114 calibration fixture. ................................................................... 228
FIGURE A-13. Maximum VSWR of calibration fixture........................................................... 229
FIGURE A-14. Insertion loss measurement. ............................................................................. 230
FIGURE A-15. CS114 alternate test setup, three phase ungrounded power system................. 231
FIGURE A-16. Circuit diagram of CS115 pulse generator....................................................... 233
FIGURE A-17. Typical CS115 calibration fixture waveform................................................... 234

TABLE
TABLE I. Absorption at normal incidence.................................................................................... 9
TABLE II. Bandwidth and measurement time. ........................................................................... 14
TABLE III. Susceptibility scanning. ........................................................................................... 15
TABLE IV. Emission and susceptibility requirements. .............................................................. 25
TABLE V. Requirement matrix................................................................................................... 26
TABLE VI. CS114 limit curves................................................................................................... 73
TABLE VII. RS103 limits. ........................................................................................................ 135
TABLE VIII. Required number of tuner positions for a reverberation chamber. ..................... 136

TABLE A-I. Susceptibility testing times................................................................................... 197

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 MIL-STD-461F

1. SCOPE
1.1 Purpose.
This standard establishes interface and associated verification requirements for the control of the
electromagnetic interference (EMI) emission and susceptibility characteristics of electronic,
electrical, and electromechanical equipment and subsystems designed or procured for use by
activities and agencies of the Department of Defense (DoD). Such equipment and subsystems
may be used independently or as an integral part of other subsystems or systems. This standard
is best suited for items that have the following features: electronic enclosures that are no larger
than an equipment rack, electrical interconnections that are discrete wiring harnesses between
enclosures, and electrical power input derived from prime power sources. This standard should
not be directly applied to items such as modules located inside electronic enclosures or entire
platforms. The principles in this standard may be useful as a basis for developing suitable
requirements for those applications. Data item requirements are also included.
1.2 Application.

1.2.1 General applicability.

The applicability of the emission and susceptibility requirements is dependent upon the types of
equipment or subsystems and their intended installations as specified herein.
1.2.2 Tailoring of requirements.
Application-specific environmental criteria may be derived from operational and engineering
analyses on equipment or subsystems being procured for use in specific systems or platforms.
When analyses reveal that the requirements in this standard are not appropriate for that
procurement, the requirements may be tailored and incorporated into the request-for-proposal,
specification, contract, order, and so forth, prior to the start of the test program. The test
procedures contained in this document should be adapted by the testing activity for each
application. The adapted test procedures should be documented in the Electromagnetic
Interference Test Procedures (EMITP) (see 6.3).
1.3 Structure.
The standard has two primary sections, the main body and the appendix. The main body
contains the interface and verification requirements of this standard. The appendix is non-
contractual and provides rationale for the requirements and guidance on their interpretation and
use. The paragraph numbering scheme for the appendix parallels the numbering for the main
body requirements except that an “A” is included (for example, A.4.2 rather than 4.2).
Occasionally, there are references in the main body to appendix material where an obvious need
exists for the appendix information to be examined.
1.4 Emission and susceptibility designations.
The emissions and susceptibility and associated test procedure requirements in this standard are
designated in accordance with an alphanumeric coding system. Each requirement is identified
by a two letter combination followed by a three digit number. The number is for reference
purposes only. The meaning of the individual letters is as follows:

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 MIL-STD-461F

C = Conducted
R = Radiated
E = Emission
S = Susceptibility

a. Conducted emissions requirements are designated by "CE---."

b. Radiated emissions requirements are designated by "RE---."
c. Conducted susceptibility requirements are designated by "CS---."
d. Radiated susceptibility requirements are designated by "RS---."
e. "---" = numerical order of requirement from 101 to 199.

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 MIL-STD-461F

2. APPLICABLE DOCUMENTS
2.1 General
The documents listed in this section are specified in sections 3, 4, or 5 of this standard. This
section does not include documents cited in other sections of this standard or recommended for
additional information or as examples. While every effort has been made to ensure the
completeness of this list, document users are cautioned that they must meet all specified
requirements of documents cited in sections 3, 4, or 5 of this standard, whether or not they are
listed.
2.2 Government documents.

2.2.1 Government documents, drawings, and publications.

The following other Government documents, drawings, and publications form a part of this
document to the extent specified herein. Unless otherwise specified, the issues of these
documents are those cited in the solicitation or contract.

DEPARTMENT OF DEFENSE (DoD)

DoDI 6055.11 – Protection of DoD Personnel from Exposure to

Radio Frequency Radiation and Military
Exempt Lasers
(Copies of this document are available online at http://www.dtic.mil/whs/directives/.)
SD-2 – Buying Commercial and Nondevelopmental
Items
(Copies of these documents are available online at http://assist.daps.dla.mil/quicksearch/ or
from the Standardization Document Order Desk, 700 Robbins Avenue, Building 4D,
Philadelphia, PA 19111-5094. [Telephone 215-697-6396].)
2.3 Non-Government publications.
The following documents form a part of this document to the extent specified herein. Unless
otherwise specified, the issues of these documents are those cited in the solicitation or contract.

AMERICAN NATIONAL STANDARDS INSTITUTE (ANSI)

ANSI/IEEE C63.2 – Standard for Electromagnetic Noise and Field
Strength Instrumentation, 10 Hz to 40 GHz -
Specifications
ANSI/IEEE C63.14 – Standard Dictionary for Technologies of
Electromagnetic Compatibility (EMC),
Electromagnetic Pulse (EMP), and Electrostatic
Discharge (ESD)

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 MIL-STD-461F

ANSI/NCSL Z540-1 – General Requirements for Calibration

Laboratories and Measuring and Test
Equipment
(Application for copies of ANSI documents should be addressed to the American National
Standards Institute, 11 West 42nd Street, New York, New York 10036 [Telephone: 212-642-4900
or Fax: 212-398-0023], http://www.ansi.org/; or the Institute of Electrical and Electronics
Engineers, Incorporated (IEEE), 445 Hoes Lane, Piscataway NJ 08855-1331 [Telephone: 800-
701-4333 or Fax: 908-981-9667], http://www.ieee.org/portal/site.)

AMERICAN SOCIETY FOR TESTING AND MATERIALS (ASTM)

ASTM SI 10 – American National Standard for Use of the
International System of Units (SI): The Modern
Metric System
(Application for copies should be addressed to the American Society for Testing and
Materials, 1916 Race Street, Philadelphia PA 19103-1187 [Telephone: 215-299-5585 or FAX:
215-977-9679], http://www.astm.org/.)

INTERNATIONAL STANDARDS ORGANIZATION

ISO 10012 – Measurement Management Systems –
Requirements for Measurement Processes and
Measuring Equipment
(Application for copies of ISO documents should be addressed to ISO, International
Organization for Standardization, 3 rue de Varembe, 1211 Geneve 20, Geneve, Switzerland
[Telephone: 41 22 734 0150], http://www.iso.org/iso/home.htm.)

SOCIETY OF AUTOMOTIVE ENGINEERS (SAE)

ARP 958 – Electromagnetic Interference Measurement
Antennas; Standard Calibration Method
(Application for copies should be addressed to the Society of Automotive Engineers,
Incorporated, 400 Commonwealth Drive, Warrendale, PA 15096 [Telephone: 412-776-4841 or
FAX: 412-776-5760], http://www.sae.org/.)
2.4 Order of precedence.
In the event of a conflict between the text of this document and the references cited herein, the
text of this document takes precedence. Nothing in this document, however, supersedes
applicable laws and regulations unless a specific exemption has been obtained.

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 MIL-STD-461F

3. DEFINITIONS
3.1 General.
The terms used in this standard are defined in ANSI C63.14. In addition, the following
definitions are applicable for the purpose of this standard.
3.2 Acronyms used in this standard.
ASW – Anti-submarine Warfare
BIT – Built-in Test
CI – Commercial Item
DoD – Department of Defense
EMC – Electromagnetic Compatibility
EME – Electromagnetic Environment
EMI – Electromagnetic Interference
EMICP – Electromagnetic Interference Control Procedures
EMITP – Electromagnetic Interference Test Procedures
EMITR – Electromagnetic Interference Test Report
ERP – Effective Radiated Power
EUT – Equipment Under Test
FCC – Federal Communication Commission
GFE – Government Furnished Equipment
ISM – Industrial, Scientific and Medical
LISN – Line Impedance Stabilization Network
NDI – Non-Developmental Item
RF – Radio Frequency
RMS – Root Mean Square
TEM – Transverse Electromagnetic
TPD – Terminal Protection Device
3.3 Above deck.
An area on ships which is not considered to be “below deck” as defined herein.
3.4 Below deck.
An area on ships which is surrounded by a metallic structure, or an area which provides
significant attenuation to electromagnetic radiation, such as the metal hull or superstructure of a
surface ship, the pressure hull of a submarine and the screened rooms in non-metallic ships.

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 MIL-STD-461F

3.5 External installation.

An equipment location on a platform which is exposed to the external electromagnetic
environment (EME), such as an aircraft cockpit which does not use electrically conductive
treatments on the canopy or windscreen.
3.6 Flight-line equipment.
Any support equipment that is attached to or used next to an aircraft during pre-flight or post-
flight operations, such as uploading or downloading data, maintenance diagnostics, or equipment
functional testing.
3.7 Internal installation.
An equipment location on a platform which is totally inside an electrically conductive structure,
such as a typical avionics bay in aluminum skin aircraft.
3.8 Metric units.
Metric units are a system of basic measures which are defined by the International System of
Units based on "Le System International d'Unites (SI)," of the International Bureau of Weights
and Measures. These units are described in ASTM SI 10.
3.9 Non-developmental item (NDI).
Non-developmental item is a broad, generic term that covers material available from a wide
variety of sources both industry and Government with little or no development effort required by
the procuring activity.
3.10 Safety critical.
A category of subsystems and equipment whose degraded performance could result in loss of life
or loss of vehicle or platform.
3.11 Test setup boundary.
The test setup boundary includes all enclosures of the Equipment Under Test (EUT) and the 2
meters of exposed interconnecting leads (except for leads which are shorter in the actual
installation) and power leads required by 4.3.8.6.

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 MIL-STD-461F

4. GENERAL REQUIREMENTS
4.1 General.
Electronic, electrical, and electromechanical equipment and subsystems shall comply with the
applicable general interface requirements in 4.2. General requirements for verification shall be
in accordance with 4.3. These general requirements are in addition to the applicable detailed
emission and susceptibility requirements and associated test procedures defined in 5.
4.2 Interface requirements.

4.2.1 Joint procurement.

Equipment or subsystems procured by one DoD activity for multi-agency use shall comply with
the requirements of the user agencies.
4.2.2 Filtering (Navy only).
The use of line-to-ground filters for EMI control shall be minimized. Such filters establish low
impedance paths for structure (common-mode) currents through the ground plane and can be a
major cause of interference in systems, platforms, or installations because the currents can
couple into other equipment using the same ground plane. If such a filter must be employed, the
line-to-ground capacitance for each line shall not exceed 0.1 microfarads (μF) for 60 Hertz (Hz)
equipment or 0.02 μF for 400 Hz equipment. For submarine DC-powered equipment and aircraft
DC-powered equipment, the filter capacitance from each line-to-ground at the user interface
shall not exceed 0.075 μF/kW of connected load. For DC loads less than 0.5 kW, the filter
capacitance shall not exceed 0.03 μF. The filtering employed shall be fully described in the
equipment or subsystem technical manual and the Electromagnetic Interference Control
Procedures (EMICP) (see 6.3).
4.2.3 Self-compatibility.
The operational performance of an equipment or subsystem shall not be degraded, nor shall it
malfunction, when all of the units or devices in the equipment or subsystem are operating
together at their designed levels of efficiency or their design capability.
4.2.4 Non-developmental items (NDI).
In accordance with the guidance provided by DoD SD-2, the requirements of this standard shall
be met when applicable and warranted by the intended installation and platform requirements.
4.2.4.1 Commercial items (CI).
4.2.4.1.1 Selected by contractor.
When it is demonstrated that a CI selected by the contractor is responsible for equipment or
subsystems failing to meet the contractual EMI requirements, either the CI shall be modified or
replaced or interference suppression measures shall be employed, so that the equipment or
subsystems meet the contractual EMI requirements.
4.2.4.1.2 Specified by procuring activity.
When it is demonstrated by the contractor that a CI specified by the procuring activity for use in
an equipment or subsystem is responsible for failure of the equipment or subsystem to meet its
contractual EMI requirements, the data indicating such failure shall be included in the

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 MIL-STD-461F

Electromagnetic Interference Test Report (EMITR) (see 6.3). No modification or replacement

shall be made unless authorized by the procuring activity.
4.2.4.2 Procurement of equipment or subsystems having met other EMI requirements.
Procurement of equipment and subsystems electrically and mechanically identical to those
previously procured by activities of DoD or other Federal agencies, or their contractors, shall
meet the EMI requirements and associated limits, as applicable in the earlier procurement, unless
otherwise specified by the Command or agency concerned.
4.2.5 Government furnished equipment (GFE).
When it is demonstrated by the contractor that a GFE is responsible for failure of an equipment
or subsystem to meet its contractual EMI requirements, the data indicating such failure shall be
included in the EMITR. No modification shall be made unless authorized by the procuring
activity.
4.2.6 Switching transients.
Switching transient emissions that result at the moment of operation of manually actuated
switching functions are exempt from the requirements of this standard. Other transient type
conditions, such as automatic sequencing following initiation by a manual switching function,
shall meet the emissions requirements of this standard.
4.2.7 Interchangeable modular equipment
The requirements of this standard are verified at the Shop Replaceable Unit, Line Replaceable
Unit, or Integrated Equipment Rack assembly level. When modular equipment such as line
replaceable modules are replaced or interchanged within the assembly, additional testing or a
similarity assessment is required. The type of assessment shall be approved by the procuring
agency.
4.3 Verification requirements.
The general requirements related to test procedures, test facilities, and equipment stated below,
together with the detailed test procedures included in 5, shall be used to determine compliance
with the applicable emission and susceptibility requirements of this standard. Any procuring
activity approved exceptions or deviations from these general requirements shall be documented
in the Electromagnetic Interference Test Procedures (EMITP) (see 6.3). Equipment intended to
be operated as a subsystem shall be tested as such to the applicable emission and susceptibility
requirements whenever practical. Formal testing is not to commence without approval of the
EMITP by the Command or agency concerned. Data that is gathered as a result of performing
tests in one electromagnetic discipline may be sufficient to satisfy requirements in another.
Therefore, to avoid unnecessary duplication, a single test program should be established with
tests for similar requirements conducted concurrently whenever possible.
4.3.1 Measurement tolerances.
Unless otherwise stated for a particular measurement, the tolerance shall be as follows:
a. Distance: ±5%
b. Frequency: ±2%
c. Amplitude, measurement receiver: ±2 dB

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 MIL-STD-461F

d. Amplitude, measurement system (includes measurement receivers, transducers, cables,

and so forth): ±3 dB
e. Time (waveforms): ±5%
f. Resistors: ±5%
g. Capacitors: ±20%
4.3.2 Shielded enclosures.
To prevent interaction between the EUT and the outside environment, shielded enclosures will
usually be required for testing. These enclosures prevent external environment signals from
contaminating emission measurements and susceptibility test signals from interfering with
electrical and electronic items in the vicinity of the test facility. Shielded enclosures shall have
adequate attenuation such that the ambient requirements of 4.3.4 are satisfied. The enclosures
shall be sufficiently large such that the EUT arrangement requirements of 4.3.8 and antenna
positioning requirements described in the individual test procedures are satisfied.
4.3.2.1 Radio Frequency (RF) absorber material.
RF absorber material (carbon impregnated foam pyramids, ferrite tiles, and so forth) shall be
used when performing electric field radiated emissions or radiated susceptibility testing inside a
shielded enclosure to reduce reflections of electromagnetic energy and to improve accuracy and
repeatability. The RF absorber shall be placed above, behind, and on both sides of the EUT, and
behind the radiating or receiving antenna as shown in Figure 1. Minimum performance of the
material shall be as specified in Table I. The manufacturer's certification of their RF absorber
material (basic material only, not installed) is acceptable.
TABLE I. Absorption at normal incidence.

Frequency Minimum absorption

80 MHz - 250 MHz 6 dB
above 250 MHz 10 dB

4.3.3 Other test sites.

If other test sites are used, the ambient requirements of 4.3.4 shall be met.
4.3.4 Ambient electromagnetic level.
During testing, the ambient electromagnetic level measured with the EUT de-energized and all
auxiliary equipment turned on shall be at least 6 dB below the allowable specified limits when
the tests are performed in a shielded enclosure. Ambient conducted levels on power leads shall
be measured with the leads disconnected from the EUT and connected to a resistive load which
draws the same rated current as the EUT. When tests are performed in a shielded enclosure and
the EUT is in compliance with required limits, the ambient profile need not be recorded in the
EMITR. When measurements are made outside a shielded enclosure, the tests shall be
performed during times and conditions when the ambient is at its lowest level. The ambient shall
be recorded in the EMITR and shall not compromise the test results.

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4.3.5 Ground plane.

The EUT shall be installed on a ground plane that simulates the actual installation. If the actual
installation is unknown or multiple installations are expected, then a metallic ground plane shall
be used. Unless otherwise specified below, ground planes shall be 2.25 square meters or larger
in area with the smaller side no less than 76 centimeters (cm). When a ground plane is not
present in the EUT installation, the EUT shall be placed on a non-conductive table.
4.3.5.1 Metallic ground plane.
When the EUT is installed on a metallic ground plane, the ground plane shall have a surface
resistance no greater than 0.1 milliohms per square. The DC resistance between metallic ground
planes and the shielded enclosure shall be 2.5 milliohms or less. The metallic ground planes
shown in Figures 2 through 5 shall be electrically bonded to the floor or wall of the basic
shielded room structure at least once every 1 meter. The metallic bond straps shall be solid and
maintain a five-to-one ratio or less in length to width. Metallic ground planes used outside a
shielded enclosure shall extend at least 1.5 meters beyond the test setup boundary in each
direction.
4.3.5.2 Composite ground plane.
When the EUT is installed on a conductive composite ground plane, the surface resistivity of the
typical installation shall be used. Composite ground planes shall be electrically bonded to the
enclosure with means suitable to the material.
4.3.6 Power source impedance.
The impedance of power sources providing input power to the EUT shall be controlled by Line
Impedance Stabilization Networks (LISNs) for all measurement procedures of this document
unless otherwise stated in a particular test procedure. LISNs shall not be used on output power
leads. The LISNs shall be located at the power source end of the exposed length of power leads
specified in 4.3.8.6.2. The LISN circuit shall be in accordance with the schematic shown in
Figure 6. The LISN impedance characteristics shall be in accordance with Figure 7. The LISN
impedance shall be measured at least annually under the following conditions:
a. The impedance shall be measured between the power output lead on the load side of the
LISN and the metal enclosure of the LISN.
b. The signal output port of the LISN shall be terminated in fifty ohms.
c. The power input terminal on the power source side of the LISN shall be unterminated.
The impedance measurement results shall be provided in the EMITR.
4.3.7 General test precautions.

4.3.7.1 Accessory equipment.

Accessory equipment used in conjunction with measurement receivers shall not degrade
measurement integrity.
4.3.7.2 Excess personnel and equipment.
The test area shall be kept free of unnecessary personnel, equipment, cable racks, and desks.
Only the equipment essential to the test being performed shall be in the test area or enclosure.
Only personnel actively involved in the test shall be permitted in the enclosure.

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4.3.7.3 Overload precautions.

Measurement receivers and transducers are subject to overload, especially receivers without
preselectors and active transducers. Periodic checks shall be performed to assure that an
overload condition does not exist. Instrumentation changes shall be implemented to correct any
overload condition.
4.3.7.4 RF hazards.
Some tests in this standard will result in electromagnetic fields which are potentially dangerous
to personnel. The permissible exposure levels in DoDI 6055.11 shall not be exceeded in areas
where personnel are present. Safety procedures and devices shall be used to prevent accidental
exposure of personnel to RF hazards.
4.3.7.5 Shock hazard.
Some of the tests require potentially hazardous voltages to be present. Extreme caution must be
taken by all personnel to assure that all safety precautions are observed.
4.3.7.6 Federal Communications Commission (FCC) restrictions.
Some of the tests require high level signals to be generated that could interfere with normal FCC
approved frequency assignments. All such testing should be conducted in a shielded enclosure.
Some open site testing may be feasible if prior FCC coordination is accomplished.
4.3.8 EUT test configurations.
The EUT shall be configured as shown in the general test setups of Figures 1 through 5 as
applicable. These setups shall be maintained during all testing unless other direction is given for
a particular test procedure.
4.3.8.1 EUT design status.
EUT hardware and software shall be representative of production. Software may be
supplemented with additional code that provides diagnostic capability to assess performance.
4.3.8.2 Bonding of EUT.
Only the provisions included in the design of the EUT shall be used to bond units such as
equipment case and mounting bases together, or to the ground plane. When bonding straps are
required, they shall be identical to those specified in the installation drawings.
4.3.8.3 Shock and vibration isolators.
EUTs shall be secured to mounting bases having shock or vibration isolators if such mounting
bases are used in the installation. The bonding straps furnished with the mounting base shall be
connected to the ground plane. When mounting bases do not have bonding straps, bonding
straps shall not be used in the test setup.
4.3.8.4 Safety grounds.
When external terminals, connector pins, or equipment grounding conductors are available for
safety ground connections and are used in the actual installation, they shall be connected to the
ground plane. Arrangement and length shall be in accordance with 4.3.8.6.1.
4.3.8.5 Orientation of EUTs.
EUTs shall be oriented such that surfaces which produce maximum radiated emissions and
respond most readily to radiated signals face the measurement antennas. Bench mounted EUTs

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 MIL-STD-461F

shall be located 10 ±2 cm from the front edge of the ground plane subject to allowances for
providing adequate room for cable arrangement as specified below.
4.3.8.6 Construction and arrangement of EUT cables.
Electrical cable assemblies shall simulate actual installation and usage. Shielded cables or
shielded leads within cables shall be used only if they have been specified in installation
requirements. Input (primary) power leads, returns, and wire grounds shall not be shielded.
Cables shall be checked against installation requirements to verify proper construction
techniques such as use of twisted pairs, shielding, and shield terminations. Details on the cable
construction used for testing shall be included in the EMITP.
4.3.8.6.1 Interconnecting leads and cables.
Individual leads shall be grouped into cables in the same manner as in the actual installation.
Total interconnecting cable lengths in the setup shall be the same as in the actual platform
installation. If a cable is longer than 10 meters, at least 10 meters shall be included. When cable
lengths are not specified for the installation, cables shall be sufficiently long to satisfy the
conditions specified below. At least the first 2 meters (except for cables which are shorter in the
actual installation) of each interconnecting cable associated with each enclosure of the EUT shall
be run parallel to the front boundary of the setup. Remaining cable lengths shall be routed to the
back of the setup and shall be placed in a zig-zagged arrangement. When the setup includes
more than one cable, individual cables shall be separated by 2 cm measured from their outer
circumference. For bench top setups using ground planes, the cable closest to the front boundary
shall be placed 10 cm from the front edge of the ground plane. All cables shall be supported
5 cm above the ground plane.
4.3.8.6.2 Input (primary) power leads.
Two meters of input power leads (including neutrals and returns) shall be routed parallel to the
front edge of the setup in the same manner as the interconnecting leads. Each input power lead,
including neutrals and returns, shall be connected to a LISN (see 4.3.6). Power leads that are
bundled as part of an interconnecting cable in the actual installation shall be separated from the
bundle and routed to the LISNs (outside the shield of shielded cables). After the 2 meter
exposed length, the power leads shall be terminated at the LISNs in as short a distance as
possible. The total length of power lead from the EUT electrical connector to the LISNs shall
not exceed 2.5 meters. All power leads shall be supported 5 cm above the ground plane. If the
power leads are twisted in the actual installation, they shall be twisted up to the LISNs.
4.3.8.7 Electrical and mechanical interfaces.
All electrical input and output interfaces shall be terminated with either the actual equipment
from the platform installation or loads which simulate the electrical properties (impedance,
grounding, balance, and so forth) present in the actual installation. Signal inputs shall be applied
to all applicable electrical interfaces to exercise EUT circuitry. EUTs with mechanical outputs
shall be suitably loaded. When variable electrical or mechanical loading is present in the actual
installation, testing shall be performed under expected worst case conditions. When active
electrical loading (such as a test set) is used, precautions shall be taken to insure the active load
meets the ambient requirements of 4.3.4 when connected to the setup, and that the active load
does not respond to susceptibility signals. Antenna ports on the EUT shall be terminated with
shielded, matched loads.

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4.3.9 Operation of EUT.

During emission measurements, the EUT shall be placed in an operating mode which produces
maximum emissions. During susceptibility testing, the EUT shall be placed in its most
susceptible operating mode. For EUTs with several available modes (including software
controlled operational modes), a sufficient number of modes shall be tested for emissions and
susceptibility such that all circuitry is evaluated. The rationale for modes selected shall be
included in the EMITP.
4.3.9.1 Operating frequencies for tunable RF equipment.
Measurements shall be performed with the EUT tuned to not less than three frequencies within
each tuning band, tuning unit, or range of fixed channels, consisting of one mid-band frequency
and a frequency within ±5 percent from each end of each band or range of channels.
4.3.9.2 Operating frequencies for spread spectrum equipment.
Operating frequency requirements for two major types of spread spectrum equipment shall be as
follows:
a. Frequency hopping. Measurements shall be performed with the EUT utilizing a hop set
which contains a minimum of 30% of the total possible frequencies. This hop set shall
be divided equally into three segments at the low, mid, and high end of the EUTs
operational frequency range.
b. Direct sequence. Measurements shall be performed with the EUT processing data at the
highest possible data transfer rate.
4.3.9.3 Susceptibility monitoring.
The EUT shall be monitored during susceptibility testing for indications of degradation or
malfunction. This monitoring is normally accomplished through the use of built-in-test (BIT),
visual displays, aural outputs, and other measurements of signal outputs and interfaces.
Monitoring of EUT performance through installation of special circuitry in the EUT is
permissible; however, these modifications shall not influence test results.
4.3.10 Use of measurement equipment.
Measurement equipment shall be as specified in the individual test procedures of this standard.
Any frequency selective measurement receiver may be used for performing the testing described
in this standard provided that the receiver characteristics (that is, sensitivity, selection of
bandwidths, detector functions, dynamic range, and frequency of operation) meet the constraints
specified in this standard and are sufficient to demonstrate compliance with the applicable limits.
Typical instrumentation characteristics may be found in ANSI C63.2.
4.3.10.1 Detector.
A peak detector shall be used for all frequency domain emission and susceptibility
measurements. This device detects the peak value of the modulation envelope in the receiver
bandpass. Measurement receivers are calibrated in terms of an equivalent Root Mean Square
(RMS) value of a sine wave that produces the same peak value. When other measurement
devices such as oscilloscopes, non-selective voltmeters, or broadband field strength sensors are
used for susceptibility testing, correction factors shall be applied for test signals to adjust the
reading to equivalent RMS values under the peak of the modulation envelope.

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 MIL-STD-461F

4.3.10.2 Computer-controlled instrumentation.

A description of the operations being directed by software for computer-controlled
instrumentation shall be included in the EMITP. Verification techniques used to demonstrate
proper performance of the software shall also be included. If commercial software is being used
then, as a minimum, the manufacturer, model and revision of the software needs to be provided.
If the software is developed in-house, then documentation needs to be included that describes the
methodology being used for the control of the test instrumentation and how the software
revisions are handled.
4.3.10.3 Emission testing.

4.3.10.3.1 Bandwidths.
The measurement receiver bandwidths listed in Table II shall be used for emission testing. These
bandwidths are specified at the 6 dB down points for the overall selectivity curve of the
receivers. Video filtering shall not be used to bandwidth limit the receiver response. If a
controlled video bandwidth is available on the measurement receiver, it shall be set to its greatest
value. Larger receiver bandwidths may be used; however, they may result in higher measured
emission levels. NO BANDWIDTH CORRECTION FACTORS SHALL BE APPLIED TO
TEST DATA DUE TO THE USE OF LARGER BANDWIDTHS.
TABLE II. Bandwidth and measurement time.

Frequency Range 6 dB Dwell Time* Minimum Measurement Time

Bandwidth Analog Measurement Receiver*
30 Hz - 1 kHz 10 Hz 0.15 sec 0.015 sec/Hz
1 kHz - 10 kHz 100 Hz 0.015 sec 0.15 sec/kHz
10 kHz - 150 kHz 1 kHz 0.015 sec 0.015 sec/kHz
150 kHz - 30 MHz 10 kHz 0.015 sec 1.5 sec/MHz
30 MHz - 1 GHz 100 kHz 0.015 sec 0.15 sec/MHz
Above 1 GHz 1 MHz 0.015 sec 15 sec/GHz

* Alternative scanning technique. Multiple faster sweeps with the use of a maximum hold
function may be used if the total scanning time is equal to or greater than the Minimum
Measurement Time defined above.

4.3.10.3.2 Emission identification.

All emissions regardless of characteristics shall be measured with the measurement receiver
bandwidths specified in Table II and compared against the applicable limits. Identification of
emissions with regard to narrowband or broadband categorization is not applicable.
4.3.10.3.3 Frequency scanning.
For emission measurements, the entire frequency range for each applicable test shall be scanned.
Minimum measurement time for analog measurement receivers during emission testing shall be
as specified in Table II. Synthesized measurement receivers shall step in one-half bandwidth

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 MIL-STD-461F

increments or less, and the measurement dwell time shall be as specified in Table II. For
equipment that operates such that potential emissions are produced at only infrequent intervals,
times for frequency scanning shall be increased as necessary to capture any emissions.
4.3.10.3.4 Emission data presentation.
Amplitude versus frequency profiles of emission data shall be automatically generated and
displayed at the time of test and shall be continuous. The displayed information shall account
for all applicable correction factors (transducers, attenuators, cable loss, and the like) and shall
include the applicable limit. Manually gathered data is not acceptable except for verification of
the validity of the output. Plots of the displayed data shall provide a minimum frequency
resolution of 1% or twice the measurement receiver bandwidth, whichever is less stringent, and
minimum amplitude resolution of 1 dB. The above resolution requirements shall be maintained
in the reported results of the EMITR.
4.3.10.4 Susceptibility testing.

4.3.10.4.1 Frequency scanning.

For susceptibility measurements, the entire frequency range for each applicable test shall be
scanned. For swept frequency susceptibility testing, frequency scan rates and frequency step
sizes of signal sources shall not exceed the values listed in Table III. The rates and step sizes are
specified in terms of a multiplier of the tuned frequency (fo) of the signal source. Analog scans
refer to signal sources which are continuously tuned. Stepped scans refer to signal sources
which are sequentially tuned to discrete frequencies. Stepped scans shall dwell at each tuned
frequency for the greater of 3 seconds or the EUT response time. Scan rates and step sizes shall
be decreased when necessary to permit observation of a response.
TABLE III. Susceptibility scanning.

Analog Scans Stepped Scans

Frequency Range Maximum Scan Rates Maximum Step Size

30 Hz - 1 MHz 0.0333fo/sec 0.05 fo

1 MHz - 30 MHz 0.00667 fo/sec 0.01 fo

30 MHz - 1 GHz 0.00333 fo/sec 0.005 fo

1 GHz - 40 GHz 0.00167 fo/sec 0.0025 fo

4.3.10.4.2 Modulation of susceptibility signals.

Susceptibility test signals for CS114 and RS103 shall be pulse modulated (on/off ratio of 40 dB
minimum) at a 1 kHz rate with a 50% duty cycle.
4.3.10.4.3 Thresholds of susceptibility.
Susceptibilities and anomalies that are not in conformance with contractual requirements are not
acceptable. However, all susceptibilities and anomalies observed during conduct of the test shall
be documented. When susceptibility indications are noted in EUT operation, a threshold level

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 MIL-STD-461F

shall be determined where the susceptible condition is no longer present. Thresholds of

susceptibility shall be determined as follows and described in the EMITR:
a. When a susceptibility condition is detected, reduce the interference signal until the EUT
recovers.
b. Reduce the interference signal by an additional 6 dB.
c. Gradually increase the interference signal until the susceptibility condition reoccurs.
The resulting level is the threshold of susceptibility.
d. Record this level, frequency range of occurrence, frequency and level of greatest
susceptibility, and other test parameters, as applicable.
4.3.11 Calibration of measuring equipment.
Test equipment and accessories required for measurement in accordance with this standard shall
be calibrated in accordance with ANSI/NCSL Z540-1 or ISO 10012 or under an approved
calibration program traceable to the National Institute for Standards and Technology. In
particular, measurement antennas, current probes, field sensors, LISNs (see Figure 7 for required
impedance), and other devices used in the measurement loop shall be calibrated at least every
2 years unless otherwise specified by the procuring activity, or when damage is apparent.
4.3.11.1 Measurement system test.
At the start of each emission test, the complete test system (including measurement receivers,
cables, attenuators, couplers, and so forth) shall be verified by injecting a known signal, as stated
in the individual test procedure, while monitoring system output for the proper indication. When
the emission test involves an uninterrupted set of repeated measurements (such as evaluating
different operating modes of the EUT) using the same measurement equipment, the measurement
system test needs to be accomplished only one time.
4.3.11.2 Antenna factors.
Factors for test antennas shall be determined in accordance with SAE ARP-958.

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 MIL-STD-461F

RF absorber placed above,

behind and on both sides of
test setup boundary, from
ceiling to ground plane

> 30 cm
TEST SETUP
BOUNDARY
> 30 cm

> 50 cm

≥30 cm
Test
Antenna

> 30 cm

RF absorber placed
behind test antenna,
from ceiling to floor

FIGURE 1. RF absorber loading diagram.

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 MIL-STD-461F

Bond strap
Access
Panel

80-90 cm
Interconnecting Cable

Ground Plane
LISNs
Source
Power

2 cm
Non-Conductive Standoff

10 cm

5 cm
2m
EUT

FIGURE 2. General test setup.

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 MIL-STD-461F

Bond strap
Access
Panel

Ground

80-90 cm
Plane
Interconnecting Cable

Non-Conductive Table
LISNs
Source
Power

2 cm

10 cm

2m
EUT

FIGURE 3. Test setup for non-conductive surface mounted EUT.

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 MIL-STD-461F

Bond Strap

Shielded Room
Ground Plane -

Floor
Enclosure

5 cm
EUT

Non-Conductive Standoff
2m
LISNs

Interconnecting Cable
Power Input
Access Panel

FIGURE 4. Test setup for free standing EUT in shielded enclosure.

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 MIL-STD-461F

ive
duct
-Con
Non tandoff Ns
S LIS
er In
Pow

eters
1.5 m um
minim

eters
1.5 m um
5 cm
minim
2m
ters
me
1.5 imum lane
min nd P
Grou
eters
1.5 m um
minim

FIGURE 5. Test setup for free standing EUT.

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 MIL-STD-461F

To 50 μH
Power To EUT
Source
8 μF 0.25 μF

To 50 Ω Termination
Or 50 Ω Input Of
Measurement
Receiver
5Ω 1k Ω

Signal Output
Port

FIGURE 6. LISN schematic.

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 MIL-STD-461F

Tolerance ±20%
100
Impedance (Ohms)

10

1
10k 100k 1M 10M 100M
Frequency (Hz)

FIGURE 7. LISN impedance.

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 MIL-STD-461F

5. DETAILED REQUIREMENTS
5.1 General.
This section specifies detailed emissions and susceptibility requirements and the associated test
procedures. Table IV is a list of the specific requirements established by this standard identified
by requirement number and title. General test procedures are included in this section. Specific
test procedures are implemented by the Government approved EMITP. All results of tests
performed to demonstrate compliance with the requirements are to be documented in the EMITR
and forwarded to the Command or agency concerned for evaluation prior to acceptance of the
equipment or subsystem. Design procedures and techniques for the control of EMI shall be
described in the EMICP. Approval of design procedures and techniques described in the EMICP
does not relieve the supplier of the responsibility of meeting the contractual emission,
susceptibility, and design requirements.
5.1.1 Units of frequency domain measurements.
All frequency domain limits are expressed in terms of equivalent Root Mean Square (RMS)
value of a sine wave as would be indicated by the output of a measurement receiver using peak
envelope detection (see 4.3.10.1).
5.2 EMI control requirements versus intended installations.
Table V summarizes the requirements for equipment and subsystems intended to be installed in,
on, or launched from various military platforms or installations. When an equipment or
subsystem is to be installed in more than one type of platform or installation, it shall comply with
the most stringent of the applicable requirements and limits. An "A" entry in the table means the
requirement is applicable. An "L" entry means the applicability of the requirement is limited as
specified in the appropriate requirement paragraphs of this standard; the limits are contained
herein. An "S" entry means the procuring activity must specify the applicability, limit, and
verification procedures in the procurement specification. Absence of an entry means the
requirement is not applicable.
5.3 Emission and susceptibility requirements, limits, and test procedures.
Individual emission or susceptibility requirements and their associated limits and test procedures
are grouped together in the following sections. The applicable frequency range and limit of
many emission and susceptibility requirements varies depending on the particular platform or
installation. The test procedures included in this section are valid for the entire frequency range
specified in the procedure; however, testing only needs to be performed over the frequency range
specified for the particular platform or installation.

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 MIL-STD-461F

TABLE IV. Emission and susceptibility requirements.

Requirement Description
CE101 Conducted Emissions, Power Leads, 30 Hz to 10 kHz
CE102 Conducted Emissions, Power Leads, 10 kHz to 10 MHz
CE106 Conducted Emissions, Antenna Terminal, 10 kHz to 40 GHz
CS101 Conducted Susceptibility, Power Leads, 30 Hz to 150 kHz
CS103 Conducted Susceptibility, Antenna Port, Intermodulation, 15 kHz to
10 GHz
CS104 Conducted Susceptibility, Antenna Port, Rejection of Undesired
Signals, 30 Hz to 20 GHz
CS105 Conducted Susceptibility, Antenna Port, Cross-Modulation, 30 Hz to
20 GHz
CS106 Conducted Susceptibility, Transients, Power Leads
CS109 Conducted Susceptibility, Structure Current, 60 Hz to 100 kHz
CS114 Conducted Susceptibility, Bulk Cable Injection, 10 kHz to 200 MHz
CS115 Conducted Susceptibility, Bulk Cable Injection, Impulse Excitation
CS116 Conducted Susceptibility, Damped Sinusoidal Transients, Cables and
Power Leads, 10 kHz to 100 MHz
RE101 Radiated Emissions, Magnetic Field, 30 Hz to 100 kHz
RE102 Radiated Emissions, Electric Field, 10 kHz to 18 GHz
RE103 Radiated Emissions, Antenna Spurious and Harmonic Outputs, 10 kHz
to 40 GHz
RS101 Radiated Susceptibility, Magnetic Field, 30 Hz to 100 kHz
RS103 Radiated Susceptibility, Electric Field, 2 MHz to 40 GHz
RS105 Radiated Susceptibility, Transient Electromagnetic Field

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 MIL-STD-461F

TABLE V. Requirement matrix.

Equipment and Subsystems Installed Requirement Applicability

In, On, or Launched From the
Following Platforms or Installations

CE101
CE102
CE106
CS101
CS103
CS104
CS105
CS106
CS109
CS114
CS115
CS116
RE101
RE102
RE103
RS101
RS103
RS105
Surface Ships A A L A S S S A L A S A A A L A A L
Submarines A A L A S S S A L A S L A A L L A L
Aircraft, Army, Including Flight Line A A L A S S S A A A A A L A A L
Aircraft, Navy L A L A S S S A A A L A L L A L
Aircraft, Air Force A L A S S S A A A A L A
Space Systems, Including Launch A L A S S S A A A A L A
Vehicles
Ground, Army A L A S S S A A A A L L A
Ground, Navy A L A S S S A A A A L A A L
Ground, Air Force A L A S S S A A A A L A

Legend:
A: Applicable
L: Limited as specified in the individual sections of this standard
S: Procuring activity must specify in procurement documentation

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 MIL-STD-461F

5.4 CE101, conducted emissions, power leads, 30 Hz to 10 kHz.

5.4.1 CE101 applicability.

This requirement is applicable for power leads, including returns, that obtain power from other
sources not part of the EUT for surface ships, submarines, Army aircraft& (including flight line)
and Navy aircraft*&
*For equipment intended to be installed on Navy aircraft, this requirement is applicable only
for aircraft with Anti-Submarine Warfare (ASW) capability.
&
For AC applications, this requirement is applicable starting at the second harmonic of the
EUT power frequency.

5.4.2 CE101 limits.

Conducted emissions on power leads shall not exceed the applicable values shown on Figures
CE101-1 through CE101-3, as appropriate, for submarines and Figure CE101-4 for Army
aircraft (including flight line) and Navy ASW aircraft.
5.4.3 CE101 test procedure.
5.4.3.1 Purpose.
This test procedure is used to verify that electromagnetic emissions from the EUT do not exceed
the specified requirements for power input leads including returns.
5.4.3.2 Test equipment.
The test equipment shall be as follows:
a. Measurement receivers
b. Current probes
c. Signal generator
d. Data recording device
e. Oscilloscope
f. Resistor (R)
g. LISNs
5.4.3.3 Setup.
The test setup shall be as follows:
a. Maintain a basic test setup for the EUT as shown and described in Figures 2 through 5
and 4.3.8. The LISN may be removed or replaced with an alternative stabilization
device when approved by the procuring activity.
b. Calibration. Configure the test setup for the measurement system check as shown in
Figure CE101-5.
c. EUT testing.
(1) Configure the test setup for compliance testing of the EUT as shown in Figure
CE101-6.

CE101
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 MIL-STD-461F

(2) Position the current probe 5 cm from the LISN.

5.4.3.4 Procedures.
The test procedures shall be as follows:
a. Turn on the measurement equipment and allow a sufficient time for stabilization.
b. Calibration. Evaluate the overall measurement system from the current probe to the
data output device.
(1) Apply a calibrated signal level, which is at least 6 dB below the applicable limit at
1 kHz, 3 kHz, and 10 kHz, to the current probe.
(2) Verify the current level, using the oscilloscope and load resistor; also, verify that
the current waveform is sinusoidal.
(3) Scan the measurement receiver for each frequency in the same manner as a
normal data scan. Verify that the data recording device indicates a level within
±3 dB of the injected level.
(4) If readings are obtained which deviate by more than ±3 dB, locate the source of
the error and correct the deficiency prior to proceeding with the testing.
c. EUT testing. Determine the conducted emissions from the EUT input power leads,
including returns.
(1) Turn on the EUT and allow sufficient time for stabilization.
(2) Select an appropriate lead for testing and clamp the current probe into position.
(3) Scan the measurement receiver over the applicable frequency range, using the
bandwidths and minimum measurement times specified in Table II.
(4) Repeat 5.4.3.4c(3) for each power lead.
5.4.3.5 Data presentation.
Data presentation shall be as follows:
a. Continuously and automatically plot amplitude versus frequency profiles on X-Y axis
outputs. Manually gathered data is not acceptable except for plot verification.
b. Display the applicable limit on each plot.
c. Provide a minimum frequency resolution of 1% or twice the measurement receiver
bandwidth, whichever is less stringent, and a minimum amplitude resolution of 1 dB for
each plot.
d. Provide plots for both the measurement and system check portions of the procedure.

CE101
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 MIL-STD-461F

100

95

90

80
Limit Level (dBμA)

76

70

60 LIMIT SHALL BE DETERMINED AS FOLLOWS:

1. For load currents ≤ 3 amperes, use the limit
curve as shown.
2. For load currents between 3 and 185
amperes, relax the limit curve by 20 log (I/3).
3. For load currents ≥ 185 amperes, relax the
50 limit curve by 35 dB.

10 100 1k 2.6 10k 100k

Frequency (Hz)

FIGURE CE101-1. CE101 limit for submarine applications, DC.

CE101
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 LIMIT SHALL BE DETERMINED AS FOLLOWS:
Input power < 1 kVA. 1. For equipment and subsystems operating < 1kVA, use the
130
limit line connecting points a, b, and c.
For equipment and subsystems with a fundamental* current
greater than 1 ampere the limit shall be relaxed as follows:
dB relaxation = 20 Log (fundamental* current).
120 a
2. For equipment and subsystems operating ≥ 1kVA, use the
limit line connecting d, b, and c.
For equipment and subsystems with a fundamental* current
greater than 1 ampere the limit shall be relaxed as follows:
dB relaxation = 20 Log (fundamental* current).
110 *Load current at the power frequency

100

30
MIL-STD-461F

Limit Level (dBμ A)

90 d
b

80
76

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Input power ≥ 1 kVA.

Check the source to verify that this is the current version before use.
c
70
120 1.92
10 100 1k 10k 100k
Frequency (Hz)

FIGURE CE101-2. CE101 limit for surface ships and submarine applications, 60 Hz.

10 December 2007
CE101
 130 Input power < 0.2 kVA
on a multi-phase source,
or < 2 amperes on a
single-phase source.
120

110 Cu
rv
e
#1

LIMIT SHALL BE DETERMINED AS FOLLOWS:

31
100 1. For equipment and subsystems operating < 0.2
kVA on a multi-phase source or < 2 amperes on
a single-phase source, use limit curve #1.
For equipment and subsystems with a Curve #2 92
MIL-STD-461F

fundamental* current greater than 1 ampere

Limit Level (dB μ A)

90 the limit shall be relaxed as follows:
dB relaxation = 20 Log (fundamental* current).
2. For equipment and subsystems operating ≥ 0.2
kVA on a multi-phase source or ≥ 2 amperes on
a single phase source, use limit curve #2.
80 Input power ≥ 0.2 kVA
For equipment and subsystems with a
fundamental* current greater than 1 ampere on a multi-phase source,
the limit shall be relaxed as follows: or ≥ 2 amperes on a

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single-phase source.

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dB relaxation = 20 Log (fundamental* current).
70 *Load current at the power frequency

10 100 1k 10k 100k

Frequency (Hz)

FIGURE CE101-3. CE101 limit for surface ships and submarine applications, 400 Hz.

10 December 2007
CE101
 MIL-STD-461F

120

CURVE #1
110

CURVE #2
Limit Level (dBμA)

100

90

80 NOMINAL EUT SOURCE VOLTAGE APPLICABLE

(AC AND DC) CURVE

ABOVE 28 VOLTS #1
70
28 VOLTS OR BELOW #2

1 10 100 1k 10k 100k

Frequency (Hz)

FIGURE CE101-4. CE101 limit for Navy ASW aircraft and Army aircraft (including
flight line) applications.

CE101
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 MIL-STD-461F

Signal
Generator

Amplifier
(As Required)

Oscilloscope R

Current Probe

Data Recorder Measurement

Receiver

FIGURE CE101-5. Measurement system check.

CE101
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 MIL-STD-461F

50 Ω Termination on
Signal Output Port
(One for Each LISN)

LISN
Power
EUT
Leads
LISN

Current Probe
5 cm

Measurement
Receiver

Data Recorder

FIGURE CE101-6. Measurement setup.

CE101
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 MIL-STD-461F

5.5 CE102, conducted emissions, power leads, 10 kHz to 10 MHz.

5.5.1 CE102 applicability.

This requirement is applicable from 10 kHz to 10 MHz for all power leads, including returns,
which obtain power from other sources not part of the EUT.
5.5.2 CE102 limits.
Conducted emissions on power leads shall not exceed the applicable values shown on Figure
CE102-1.
5.5.3 CE102 test procedure.
5.5.3.1 Purpose.
This test procedure is used to verify that electromagnetic emissions from the EUT do not exceed
the specified requirements for power input leads, including returns.
5.5.3.2 Test equipment.
The test equipment shall be as follows:
a. Measurement receiver
b. Data recording device
c. Signal generator
d. Attenuator, 20 dB, 50 ohm
e. Oscilloscope
f. LISNs
5.5.3.3 Setup.
The test setup shall be as follows:
a. Maintain a basic test setup for the EUT as shown and described in Figures 2 through 5
and 4.3.8.
b. Calibration.
(1) Configure the test setup for the measurement system check as shown in Figure
CE102-2. Ensure that the EUT power source is turned off.
(2) Connect the measurement receiver to the 20 dB attenuator on the signal output
port of the LISN.
c. EUT testing.
(1) Configure the test setup for compliance testing of the EUT as shown in Figure
CE102-3.
(2) Connect the measurement receiver to the 20 dB attenuator on the signal output
port of the LISN.
5.5.3.4 Procedures.
The test procedures shall be as follows:

CE102
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 MIL-STD-461F

a. Calibration. Perform the measurement system check using the measurement system
check setup of Figure CE102-2.
(1) Turn on the measurement equipment and allow a sufficient time for stabilization.
(2) Apply a signal level that is at least 6 dB below the limit at 10 kHz, 100 kHz, 2
MHz and 10 MHz to the power output terminal of the LISN. At 10 kHz and 100
kHz, use an oscilloscope to calibrate the signal level and verify that it is
sinusoidal. At 2 MHz and 10 MHz, use a calibrated output level directly from a
50 Ω signal generator.
(3) Scan the measurement receiver for each frequency in the same manner as a
normal data scan. Verify that the measurement receiver indicates a level within
±3 dB of the injected level. Correction factors shall be applied for the 20 dB
attenuator and the voltage drop due to the LISN 0.25 μF coupling capacitor (see
Figure 6).
(4) If readings are obtained which deviate by more than ±3 dB, locate the source of
the error and correct the deficiency prior to proceeding with the testing.
(5) Repeat 5.5.3.4a(2) through 5.5.3.4a(4) for each LISN.
b. EUT testing. Perform emission data scans using the measurement setup of Figure
CE102-3.
(1) Turn on the EUT and allow a sufficient time for stabilization.
(2) Select an appropriate lead for testing.
(3) Scan the measurement receiver over the applicable frequency range, using the
bandwidths and minimum measurement times in the Table II.
(4) Repeat 5.5.3.4b(2) and 5.5.3.4b(3) for each power lead.
5.5.3.5 Data presentation.
Data presentation shall be as follows:
a. Continuously and automatically plot amplitude versus frequency profiles on X-Y axis
outputs. Manually gathered data is not acceptable except for plot verification.
b. Display the applicable limit on each plot.
c. Provide a minimum frequency resolution of 1% or twice the measurement receiver
bandwidth, whichever is less stringent, and a minimum amplitude resolution of 1 dB for
each plot.
d. Provide plots for both the measurement system check and measurement portions of the
procedure.

CE102
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 MIL-STD-461F

NOMINAL EUT LIMIT

SOURCE VOLTAGE (AC&DC) RELAXATION
100
28V BASIC CURVE
115V 6dB
94 220V 9dB
270V 10dB
90 =/> 440V 12dB
Limit Level (dBμV)

80

70

BASIC CURVE
60

50

10k 100k 1M 10M 100M

Frequency (Hz)

FIGURE CE102-1. CE102 limit (EUT power leads, AC and DC) for all applications.

CE102
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 MIL-STD-461F

Coaxial
"T" Connector
Power
Input
(Off)
LISN Signal
Generator

Oscilloscope
Signal
Output 10 kHz and 100 kHz
Port Calibration Only

Measurement
20 dB Attenuator
Receiver

Data
Recording
Device

FIGURE CE102-2. Measurement system check setup.

CE102
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 MIL-STD-461F

50 Ω
Termination Power
Lead Power Cable
Power
Input
LISN
EUT
LISN
Signal
20 dB
Output
Attenuator Power
Port
Lead

Measurement
Receiver

Data
Recording
Device

FIGURE CE102-3. Measurement setup.

CE102
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 MIL-STD-461F

5.6 CE106, conducted emissions, antenna terminal, 10 kHz to 40 GHz.

5.6.1 CE106 applicability.

This requirement is applicable to the antenna terminals of transmitters, receivers, and amplifiers.
The requirement is not applicable to equipment designed with antennas permanently mounted to
the EUT. The transmit mode portion of this requirement is not applicable within the bandwidth
of the EUT transmitted signal or within ±5 percent of the fundamental frequency, whichever is
larger. Depending on the operating frequency range of the EUT, the start frequency of the test is
as follows:
EUT Operating Frequency Range Start Frequency of Test
10 kHz to 3 MHz 10 kHz
3 MHz to 300 MHz 100 kHz
300 MHz to 3 GHz 1 MHz
3 GHz to 40 GHz 10 MHz
The end frequency of the test is 40 GHz or twenty times the highest generated or received
frequency within the EUT, whichever is less. For equipment using waveguide, the requirement
does not apply below eight-tenths of the waveguide's cutoff frequency. RE103 may be used as
an alternative for CE106 for testing transmitters with their operational antennas. RE102 is
applicable for emissions from antennas in receive and standby modes for equipment designed
with antennas permanently mounted to the EUT.
5.6.2 CE106 limits.
Conducted emissions at the EUT antenna terminal shall not exceed the values given below.
a. Receivers: 34 dBμV
b. Transmitters and amplifiers (standby mode): 34 dBμV
c. Transmitters and amplifiers (transmit mode): Harmonics, except the second and third,
and all other spurious emissions shall be at least 80 dB down from the level at the
fundamental. The second and third harmonics shall be suppressed to a level of -20 dBm
or 80 dB below the fundamental, whichever requires less suppression.
5.6.3 CE106 test procedure.
5.6.3.1 Purpose.
This test procedure is used to verify that conducted emissions appearing at the antenna terminal
of the EUT do not exceed specified requirements.
5.6.3.2 Test equipment.
The test equipment shall be as follows:
a. Measurement receiver
b. Attenuators, 50 ohm
c. Rejection networks

CE106
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 MIL-STD-461F

d. Directional couplers
e. Dummy loads, 50 ohm
f. Signal generators. For amplifier testing, a signal generator is required to drive the
amplifier that provides the modulation used in the intended application and that has
spurious and harmonic outputs that are down at least 6 dB greater than the applicable
limit.
g. Data recording device
5.6.3.3 Setup.
It is not necessary to maintain the basic test setup for the EUT as shown and described in Figures
2 through 5 and 4.3.8. The test setup shall be as follows:
a. Calibration. Configure the test setup for the signal generator path shown in Figures
CE106-1 through CE106-3 as applicable. The choice of Figure CE106-1 or CE106-2 is
dependent upon the capability of the measuring equipment to handle the transmitter
power.
b. EUT Testing. Configure the test setup for the EUT path shown in Figures CE106-1
through CE106-3 as applicable. The choice of Figure CE106-1 or CE106-2 is
dependent upon the capability of the measuring equipment to handle the transmitter
power.
5.6.3.4 Procedures.

5.6.3.4.1 Transmit mode for transmitters and amplifiers.

The test procedure shall be as follows:
a. Turn on the measurement equipment and allow a sufficient time for stabilization.
b. Calibration.
(1) Apply a known calibrated signal level from the signal generator through the
system check path at a mid-band fundamental frequency (fo).
(2) Scan the measurement receiver in the same manner as a normal data scan. Verify
the measurement receiver detects a level within ±3 dB of the expected signal.
(3) If readings are obtained which deviate by more than ±3 dB, locate the source of
the error and correct the deficiency prior to proceeding with the test.
(4) Repeat 5.6.3.4.1b(1) through 5.6.3.4.1b(3) at the end points of the frequency
range of test.
c. EUT Testing.
(1) Turn on the EUT and allow sufficient time for stabilization.
(2) For transmitters, tune the EUT to the desired test frequency and apply the
appropriate modulation for the EUT as indicated in the equipment specification.
For amplifiers, apply an input signal to the EUT that has the appropriate
frequency, power level, and modulation as indicated in the equipment
specification. For transmitters and amplifiers for which these parameters vary,

CE106
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 MIL-STD-461F

test parameters shall be chosen such that the worst case emissions spectrum will
result.
(3) Use the measurement path to complete the rest of this procedure.
(4) Tune the test equipment to the operating frequency (fo) of the EUT and adjust for
maximum indication.
(5) Record the power level of the fundamental frequency (fo) and the measurement
receiver bandwidth.
(6) Insert the fundamental frequency rejection network, when applicable.
(7) Scan the frequency range of interest and record the level of all harmonics and
spurious emissions. Add all correction factors for cable loss, attenuators and
rejection networks. Maintain the same measurement receiver bandwidth used to
measure the power level of the fundamental frequency (fo) in 5.6.3.4.1c(5).
(8) Verify spurious outputs are from the EUT and not spurious responses of the
measurement system.
(9) Repeat 5.6.3.4.1c(2) through 5.6.3.4.1c(8) for other frequencies as required by
4.3.9.1 and 4.3.9.2.
(10) Determine measurement path losses at each spurious frequency as follows:
(a) Replace the EUT with a signal generator.
(b) Retain all couplers and rejection networks in the measurement path.
(c) Determine the losses through the measurement path. The value of attenuators
may be reduced to facilitate the end-to-end check with a low level signal
generator.
5.6.3.4.2 Receivers and stand-by mode for transmitters and amplifiers.
The test procedure shall be as follows:
a. Turn on the measurement equipment and allow a sufficient time for stabilization.
b. Calibration.
(1) Apply a calibrated signal level, which is 6 dB below the applicable limit, from the
signal generator through the system check path at a midpoint test frequency.
(2) Scan the measurement receiver in the same manner as a normal data scan. Verify
the measurement receiver detects a level within ±3 dB of the injected signal.
(3) If readings are obtained which deviate by more than ±3 dB, locate the source of
the error and correct the deficiency prior to proceeding with the test.
(4) Repeat 5.6.3.4.2b(1) through 5.6.3.4.2b(3) at the end points of the frequency
range of test.
c. EUT Testing.
(1) Turn on the EUT and allow sufficient time for stabilization.

CE106
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 MIL-STD-461F

(2) Tune the EUT to the desired test frequency and use the measurement path to
complete the rest of this procedure.
(3) Scan the measurement receiver over the applicable frequency range, using the
bandwidths and minimum measurement times of Table II.
(4) Repeat 5.6.3.4.2c(2) and 5.6.3.4.2c(3) for other frequencies as required by 4.3.9.1
and 4.3.9.2.
5.6.3.5 Data presentation.

5.6.3.5.1 Transmit mode for transmitters and amplifiers.

The data presentation shall be as follows:
a. Continuously and automatically plot amplitude versus frequency profiles for each tuned
frequency. Manually gathered data is not acceptable except for plot verification.
b. Provide a minimum frequency resolution of 1% or twice the measurement receiver
bandwidth, whichever is less stringent, and a minimum amplitude resolution of 1 dB for
each plot.
c. Provide tabular data showing fo and frequencies of all harmonics and spurious
emissions measured, power level of the fundamental and all harmonics and spurious
emissions, dB down level, and all correction factors including cable loss, attenuator
pads, and insertion loss of rejection networks.
d. The relative dB down level is determined by subtracting the level in 5.6.3.4.1c(7) from
that obtained in 5.6.3.4.1c(5).
5.6.3.5.2 Receivers and stand-by mode for transmitters and amplifiers.
The data presentation shall be as follows:
a. Continuously and automatically plot amplitude versus frequency profiles for each tuned
frequency. Manually gathered data is not acceptable except for plot verification.
b. Display the applicable limit on each plot.
c. Provide a minimum frequency resolution of 1% or twice the measurement receiver
bandwidth, whichever is less stringent, and a minimum amplitude resolution of 1 dB for
each plot.
d. Provide plots for both the measurement and system check portions of the procedure.

CE106
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 MIL-STD-461F

Transmitter Amplifier Signal

EUT EUT Generator

Path for
Measurement
Signal
Generator

Path for
System Check

Attenuator

Rejection
If Required Network

Measurement
Receiver

FIGURE CE106-1. Setup for low power transmitters and amplifiers.

CE106
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 MIL-STD-461F

Transmitter Amplifier Signal

EUT EUT Generator

Path for
Measurement
Signal
Generator

Path for
System Check

Dummy Load
or Coupler
Shielded
Antenna

Attenuator

Rejection
If Required Network

Measurement
Receiver

FIGURE CE106-2. Setup for high power transmitters and amplifiers.

CE106
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 MIL-STD-461F

EUT

Path for
Measurement
Signal
Generator

Path for Attenuator

System Check

Measurement
Receiver

Data
Recording
Device

FIGURE CE106-3. Setup for receivers and stand-by mode for transmitters and amplifiers.

CE106
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 MIL-STD-461F

5.7 CS101, conducted susceptibility, power leads, 30 Hz to 150 kHz.

5.7.1 CS101 applicability.

This requirement is applicable to equipment and subsystem AC, limited to current draws ≤ 100
amperes per phase, and DC input power leads, not including returns. If the EUT is DC operated,
this requirement is applicable over the frequency range of 30 Hz to 150 kHz. If the EUT is AC
operated, this requirement is applicable starting from the second harmonic of the EUT power
frequency and extending to 150 kHz.
5.7.2 CS101 limit.
The EUT shall not exhibit any malfunction, degradation of performance, or deviation from
specified indications, beyond the tolerances indicated in the individual equipment or subsystem
specification, when subjected to a test signal with voltage levels as specified in Figure CS101-1.
The requirement is also met when the power source is adjusted to dissipate the power level
shown in Figure CS101-2 in a 0.5 ohm load and the EUT is not susceptible.
5.7.3 CS101 test procedure.

5.7.3.1 Purpose.
This test procedure is used to verify the ability of the EUT to withstand signals coupled onto
input power leads.
5.7.3.2 Test equipment.
The test equipment shall be as follows:
a. Signal generator
b. Power amplifier
c. Oscilloscope
d. Coupling transformer
e. Capacitor, 10 μF
f. Isolation transformer
g. Resistor, 0.5 ohm
h. LISNs
5.7.3.3 Setup.
The test setup shall be as follows:
a. Maintain a basic test setup for the EUT as shown and described in Figures 2 through 5
and 4.3.8.
b. Calibration. Configure the test equipment in accordance with Figure CS101-3. Set up
the oscilloscope to monitor the voltage across the 0.5 ohm resistor.
c. EUT testing.
(1) For DC or single phase AC power, configure the test equipment as shown in
Figure CS101-4.

CS101
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 MIL-STD-461F

(2) For three phase ungrounded power, configure the test setup as shown in Figure
CS101-5.
(3) For three phase wye power (four power leads), configure the test setup as shown
in Figure CS101-6.
5.7.3.4 Procedures.
The test procedures shall be as follows:
a. Turn on the measurement equipment and allow sufficient time for stabilization.
b. Calibration.
(1) Set the signal generator to the lowest test frequency.
(2) Increase the applied signal until the oscilloscope indicates the voltage level
corresponding to the maximum required power level specified for the limit in
Figure CS101-2. Verify the output waveform is sinusoidal.
(3) Record the setting of the signal source.
(4) Scan the required frequency range for testing and record the signal source setting
needed to maintain the required power level.
c. EUT Testing.
(1) Turn on the EUT and allow sufficient time for stabilization. CAUTION: Exercise
care when performing this test since the "safety ground" of the oscilloscope is
disconnected due to the isolation transformer and a shock hazard may be present.
(2) Set the signal generator to the lowest test frequency. Increase the signal level
until the required voltage or power level is reached on the power lead. (Note:
Power is limited to the level calibrated in 5.7.3.4b(2).)
(3) While maintaining at least the required signal level, scan through the required
frequency range at a rate no greater than specified in Table III.
(4) Susceptibility evaluation.
(a) Monitor the EUT for degradation of performance.
(b) If susceptibility is noted, determine the threshold level in accordance with
4.3.10.4.3 and verify that it is above the limit.
(5) Repeat 5.7.3.4c(2) through 5.7.3.4c(4) for each power lead, as required. For three
phase ungrounded power, the measurements shall be made according to the
following table:

Coupling Transformer Voltage Measurement

in Line From
A A to B
B B to C
C C to A

CS101
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 MIL-STD-461F

For three phase wye power (four leads) the measurements shall be made according to
the following table:

Coupling Transformer Voltage Measurement

in Line From
A A to neutral
B B to neutral
C C to neutral

5.7.3.5 Data presentation.

Data presentation shall be as follows:
a. Provide graphical or tabular data showing the frequencies and amplitudes at which the
test was conducted for each lead.
b. Provide data on any susceptibility thresholds and the associated frequencies that were
determined for each power lead.
c. Provide indications of compliance with the applicable requirements for the
susceptibility evaluation specified in 5.7.3.4c for each lead.

CS101
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 MIL-STD-461F

150

140
CURVE #1
136

130
CURVE #2
126
Limit Level (dBμV)

120

110
106.5

NOMINAL EUT APPLICABLE

100 SOURCE VOLTAGE CURVE
96.5
ABOVE 28 VOLTS #1
90 28 VOLTS OR BELOW #2

80
150k
10 100 1k 10k 100k 1M
Frequency (Hz)

FIGURE CS101-1. CS101 voltage limit for all applications.

CS101
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 MIL-STD-461F

100
80

10
Limit level (Watts)

0.1 0.09

0.01 150k
10 100 1k 10k 100k 1M
Frequency (Hz)

FIGURE CS101-2. CS101 power limit for all applications.

CS101
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 MIL-STD-461F

Signal
Generator

Power
Amplifier

Coupling
Transformer

Oscilloscope 0.5 Ω

FIGURE CS101-3. Calibration.

CS101
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 MIL-STD-461F

Return
High

Power
Inputs
LISN

10 μF
Transformer
Generator

Amplifier

Coupling
Power
Signal

Oscilloscope
Transformer
Isolation

Power
Lead
Stimulation

Equipment
Monitoring

EUT
and

FIGURE CS101-4. Signal injection, DC or single phase AC.

CS101
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 MIL-STD-461F

C
A
B

Power
Inputs
LISN

10 μF
10 μF
10 μF
Transformer
Generator

Coupling
Amplifier
Power
Signal

Oscilloscope
Transformer
Isolation

Power
Lead
Stimulation

Equipment
Monitoring

EUT
and

FIGURE CS101-5. Signal injection, 3-phase ungrounded.

CS101
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 MIL-STD-461F

Neutral
C
A
B

Power
Inputs
LISN

10 μF
10 μF
Transformer
Generator

Coupling
Amplifier
Power
Signal

10 μF
Oscilloscope
Transformer
Isolation

Power
Lead
Stimulation

Equipment
Monitoring

EUT
and

FIGURE CS101-6. Signal injection, 3-phase wye.

CS101
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 MIL-STD-461F

5.8 CS103, conducted susceptibility, antenna port, intermodulation, 15 kHz to 10 GHz.

5.8.1 CS103 applicability.

This receiver front-end susceptibility requirement is applicable to equipment and subsystems,
such as communications receivers, RF amplifiers, transceivers, radar receivers, acoustic
receivers, and electronic warfare receivers as specified in the individual procurement
specification.
5.8.2 CS103 limit.
The EUT shall not exhibit any intermodulation products beyond specified tolerances when
subjected to the limit requirement provided in the individual procurement specification.
5.8.3 CS103 test procedures.

5.8.3.1 Purpose.
This test procedure is used to determine the presence of intermodulation products that may be
caused by undesired signals at the EUT antenna input terminals.
5.8.3.2 Test requirements.
The required test equipment, setup, procedures, and data presentation shall be determined on a
case-by-case basis in accordance with the guidance provided in A.5.8 of the appendix of this
standard.

CS103
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 MIL-STD-461F

5.9 CS104, conducted susceptibility, antenna port, rejection of undesired signals, 30 Hz to

20 GHz.

5.9.1 CS104 applicability.

This receiver front-end susceptibility requirement is applicable to equipment and subsystems,
such as communications receivers, RF amplifiers, transceivers, radar receivers, acoustic
receivers, and electronic warfare receivers as specified in the individual procurement
specification.
5.9.2 CS104 limit.
The EUT shall not exhibit any undesired response beyond specified tolerances when subjected to
the limit requirement provided in the individual procurement specification.
5.9.3 CS104 test procedures.
5.9.3.1 Purpose.
This test procedure is used to determine the presence of spurious responses that may be caused
by undesired signals at the EUT antenna input terminals.
5.9.3.2 Test requirements.
The required test equipment, setup, procedures, and data presentation shall be determined on a
case-by-case basis in accordance with the guidance provided in A.5.9 of the appendix of this
standard.

CS104
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 MIL-STD-461F

5.10 CS105, conducted susceptibility, antenna port, cross modulation, 30 Hz to 20 GHz.

5.10.1 CS105 applicability.

This receiver front-end susceptibility requirement is applicable only to receivers that normally
process amplitude-modulated RF signals, as specified in the individual procurement
specification.
5.10.2 CS105 limit.
The EUT shall not exhibit any undesired response, due to cross modulation, beyond specified
tolerances when subjected to the limit requirement provided in the individual procurement
specification.
5.10.3 CS105 test procedures.

5.10.3.1 Purpose.
This test procedure is used to determine the presence of cross-modulation products that may be
caused by undesired signals at the EUT antenna terminals.
5.10.3.2 Test requirements.
The required test equipment, setup, procedures, and data presentation shall be determined in
accordance with the guidance provided in A.5.10 of the appendix of this standard.

CS105
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 MIL-STD-461F

5.11 CS106, conducted susceptibility, transients, power leads.

5.11.1 CS106 Applicability.

This requirement is applicable to submarine and surface ship equipment and subsystem AC and
DC input power leads, not including grounds and neutrals.
5.11.2 CS106 limit.
The EUT shall not exhibit any malfunction, degradation of performance, or deviation from
specified indications, beyond the tolerances indicated in the individual equipment or subsystem
specification, when subjected to a test signal with voltage levels as specified in Figure CS106-1.
5.11.3 CS106 test procedure.
5.11.3.1 Purpose.
This test procedure is used to verify the ability of the EUT to withstand transients coupled onto
input power leads.
5.11.3.2 Test equipment.
The test equipment shall be as follows:
a. Transient generator, ≤ 2 ohm source impedance
b. Capacitor, 10 μf
c. Oscilloscope
d. Resistor, 5 ohm (non-inductive)
e. Isolation transformer
5.11.3.3 Setup.
The test setup shall be as follows:
a. Maintain a basic test setup for the EUT as shown and described in Figures 2 through 5
and 4.3.8.
b. Calibration. Configure the test equipment in accordance with Figure CS106-2. Set up
the oscilloscope to monitor the specified voltage across the 5 ohm non-inductive
resistor.
c. EUT testing.
(1) For DC or single phase AC power, configure the test equipment as shown in
Figure CS106-3.
(2) For three phase ungrounded power, configure the test setup as shown in Figure
CS106-4.
(3) For three phase wye power (four power leads), configure the test setup as shown
in Figure CS106-5.
5.11.3.4 Procedures.
Test procedures shall be as follows:
a. Turn on the measurement equipment and allow sufficient time for stabilization.

CS106
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 MIL-STD-461F

b. Calibration.
(1) Set the transient generator to minimum output.
(2) Increase the applied signal until the oscilloscope indicates the voltage level
corresponding to the limit. Verify the output waveform and pulse width.
(3) Record the setting of the transient generator.
c. EUT Testing.
(1) Turn on the EUT and allow sufficient time for stabilization. CAUTION: Exercise
care when performing this test since the "safety ground" of the oscilloscope is
disconnected due to the isolation transformer and a shock hazard may be present.
(2) Set the transient generator to minimum output. Increase the signal level until the
required voltage is reached on the power lead or spike generator calibration set
point is obtained. Note: Calibration set point is that obtained in 5.11.3.4b(2).
(3) While maintaining at least the required signal level, apply transient pulses to the
test sample’s ungrounded input lines at a pulse repetition rate of between 5 and 10
pulses per second for not less than 5 minutes.
(4) Susceptibility evaluation.
(a) Monitor the EUT for degradation of performance.
(b) If susceptibility is noted, determine and record its threshold level and phase
position on the AC waveform in accordance with 4.3.10.4.3 and verify that it
is above the limit.
(5) Repeat 5.11.3.4c(1) through 5.11.3.4c(4) for each power lead and test condition,
as required.
5.11.3.5 Data presentation.
Data presentation shall be as follows:
a. Provide oscilloscope photographs of the calibration waveform obtained in 5.11.3.4b.(2).
b. Provide oscilloscope photographs of the injected waveform for each lead.
c. Provide data on any susceptibility thresholds that were determined for each power lead.
d. Provide indications of compliance with the applicable requirements for the
susceptibility evaluation listed in 5.11.3.5c for each lead.

CS106
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 MIL-STD-461F

amplitude

Vpeak

tr time
tf Vsag

td
tsag

Where:
Vpeak = 400 volt peak
tr = 1.5 μsec, ± 0.5 μsec
tf = 3.5 μsec, ± 0.5 μsec
td = 5.0 μsec, ± 22%
Vsag ≤ 120 volt peak (maximum)
tsag ≤ 20 μsec

Measured across a 5.0 ohm non-inductive resistor.

FIGURE CS106-1. CS106 voltage limit.

CS106
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 MIL-STD-461F

Transient
Generator

Oscilloscope 5Ω

FIGURE CS106-2. Calibration.

CS106
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 MIL-STD-461F

Return
High

Power
Inputs
LISNs

10 μf
Generator
Spike

Power Leads
Oscilloscope
Transformer
Isolation

Equipment
Simulation

Monitoring

EUT
and

FIGURE CS106-3. Signal injection, DC or single phase AC.

CS106
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 MIL-STD-461F

Power
C

Inputs
A

B
LISNs

10 μf
Generator

10 μf
10 μf
Spike

Power Leads
Oscilloscope
Transformer
Isolation

Equipment
Monitoring
Simulation

EUT
and

FIGURE CS106-4. Signal injection, 3-phase ungrounded.

CS106
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 MIL-STD-461F

Neutral
Power
C

Inputs
A

B
LISNs

10 μf
10 μf
Generator

10 μf
Spike

Power Leads
Oscilloscope
Transformer
Isolation

Equipment
Simulation

Monitoring

EUT
and

FIGURE CS106-5. Signal injection, 3-phase wye.

CS106
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 MIL-STD-461F

5.12 CS109, conducted susceptibility, structure current, 60 Hz to 100 kHz.

5.12.1 CS109 applicability.

This requirement is applicable to equipment and subsystems that have an operating frequency of
100 kHz or less and an operating sensitivity of 1 μV or better (such as 0.5 μV). Handheld
equipment is exempt from this requirement.
5.12.2 CS109 limit.
The EUT shall not exhibit any malfunction, degradation of performance, or deviation from
specified indications, beyond the tolerances indicated in the individual equipment or subsystem
specification, when subjected to the values shown on Figure CS109-1.
5.12.3 CS109 test procedures.

5.12.3.1 Purpose.
This test procedure is used to verify the ability of the EUT to withstand structure currents.
5.12.3.2 Test equipment.
The test equipment shall be as follows:
a. Signal generator
b. Amplifier (if required)
c. Isolation transformers
d. Current probe
e. Measurement receiver
f. Resistor, 0.5 ohm
g. Coupling transformer
5.12.3.3 Setup.
The test setup shall be as follows:
a. It is not necessary to maintain the basic test setup for the EUT as shown and described
in Figures 2 through 5 and 4.3.8.
b. Calibration. No special calibration is required.
c. EUT testing.
(1) As shown in Figure CS109-2, configure the EUT and the test equipment
(including the test signal source, the test current measurement equipment, and the
equipment required for operating the EUT or measuring performance
degradation) to establish a single-point ground for the test setup using the EUT
ground terminal.
(a) Using isolation transformers, isolate all AC power sources. For DC power,
isolation transformers are not applicable.
(b) Disconnect the safety ground leads of all input power cables.

CS109
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 MIL-STD-461F

(c) Place the EUT and the test equipment on non-conductive surfaces to enable a
single point ground to be established.
(2) The test points for the injected currents shall be as follows:
(a) Equipment that will not be rack mounted: At diagonal extremes across only
the mounting surface.
(b) Rack mounted equipment: At diagonal extremes across all surfaces of the
equipment.
(c) Deck resting equipment: At diagonal extremes across all surfaces of the
equipment.
(d) Bulkhead mounted equipment: At diagonal extremes across rear surface of
the equipment.
(e) Cables (all mounting methods): Between cable armor, which is terminated at
the EUT, and the single point ground established for the test setup. This
requirement shall also apply to cable shields and conduit, unless they have a
single point ground.
(3) Connect the signal generator and resistor to a selected set of test points.
Attachment to the test points shall be by conductors that are perpendicular to the
test surface for a length of at least 50 cm.
5.12.3.4 Procedures.
The test procedures shall be as follows:
a. Turn on the EUT and measurement equipment and allow sufficient time for
stabilization.
b. Set the signal generator to the lowest required frequency. Adjust the signal generator to
the required level as a minimum. Monitor the current with the current probe and
measurement receiver.
c. Scan the signal generator over the required frequency range in accordance with Table
III while maintaining the current level at least to the level specified in the applicable
limit. Monitor the EUT for susceptibility.
d. If susceptibility is noted, determine the threshold level in accordance with 4.3.10.4.3
and verify that it is above the applicable limit.
e. Repeat 5.12.3.4b through 5.12.3.4d for each diagonal set of test points on each surface
of the EUT to be tested.
5.12.3.5 Data presentation.
Data presentation shall be as follows:
a. Provide a table showing the mode of operation, susceptible frequency, current threshold
level, current limit level, and susceptible test points.
b. Provide a diagram of the EUT showing the location of each set of test points.

CS109
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 MIL-STD-461F

130

120

110

103
Limit Level (dBμA)

100

90

80

70

60

10 100 1k 10k 100k 1M

Frequency (Hz)

FIGURE CS109-1. CS109 limit.

CS109
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 MIL-STD-461F

AC DC
Power Power
Input Input

EUT
Ground Isolation
Terminal Transformer

Single-Point
Ground

EUT
Conductors must be
perpendicular to surface
for at least 50 cm
0.5 Ω

Current
Probe Coupling
Transformer

Measurement
Receiver
Amplifier

Signal
Generator

FIGURE CS109-2. Test configuration.

CS109
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 MIL-STD-461F

5.13 CS114, conducted susceptibility, bulk cable injection, 10 kHz to 200 MHz.

5.13.1 CS114 applicability.

This requirement is applicable to all interconnecting cables, including power cables.
5.13.2 CS114 limit.
The EUT shall not exhibit any malfunction, degradation of performance, or deviation from
specified indications beyond the tolerances indicated in the individual equipment or subsystem
specification, when subjected to an injection probe drive level which has been pre-calibrated to
the appropriate current limit shown in Figure CS114-1 and is modulated as specified below. The
appropriate limit curve in Figure CS114-1 shall be selected from Table VI. For EUTs intended
to be installed on ships or submarines, an additional common mode limit of 77 dBμA is
applicable from 4 kHz to 1 MHz on complete power cables (highs and returns - common mode
test). Requirements are also met if the EUT is not susceptible at forward power levels sensed by
the directional coupler that are below those determined during calibration provided that the
actual current induced in the cable under test is 6 dB or greater than the calibration limit.
The requirement is not applicable for coaxial cables to antenna ports of antenna-connected
receivers except for surface ships and submarines.
5.13.3 CS114 test procedures.

5.13.3.1 Purpose.
This test procedure is used to verify the ability of the EUT to withstand RF signals coupled onto
EUT associated cabling.
5.13.3.2 Test equipment.
The test equipment shall be as follows:
a. Measurement receivers
b. Current injection probes (maximum insertion loss shown in Figure CS114-2, minimum
insertion loss is recommended, not required)
c. Current probes
d. Calibration fixture: coaxial transmission line with 50 ohm characteristic impedance,
coaxial connections on both ends, and space for an injection probe around the center
conductor.
e. Directional couplers
f. Signal generators
g. Plotter
h. Attenuators, 50 ohm
i. Coaxial loads, 50 ohm
j. Power amplifiers
k. LISNs

CS114
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 MIL-STD-461F

5.13.3.3 Setup.
The test setup shall be as follows:
a. Maintain a basic test setup for the EUT as shown and described in Figures 2 through 5
and 4.3.8.
b. Calibration. Configure the test equipment in accordance with Figure CS114-3 for
calibrating injection probes.
(1) Place the injection probe around the center conductor of the calibration fixture.
(2) Terminate one end of the calibration fixture with a 50 ohm load and terminate the
other end with an attenuator connected to measurement receiver A.
c. EUT Testing. Configure the test equipment as shown in Figure CS114-4 for testing of
the EUT.
(1) Place the injection and monitor probes around a cable bundle interfacing with
EUT connector.
(2) To minimize errors, maintain the same signal circuit that was used for calibration
between the attenuator at the calibration fixture (oscilloscope, coaxial cables,
bulkhead connectors, additional attenuators, etc.) and connect the circuit to the
monitor probe. Additional attenuation may be used, if necessary.
(3) Locate the monitor probe 5 cm from the connector. If the overall length of the
connector and backshell exceeds 5 cm, position the monitor probe as close to the
connector's backshell as possible.
(4) Position the injection probe 5 cm from the monitor probe.
5.13.3.4 Procedures.
The test procedures shall be as follows:
a. Turn on the measurement equipment and allow sufficient time for stabilization.
b. Calibration. Perform the following procedures using the calibration setup.
(1) Set the signal generator to 10 kHz, unmodulated.
(2) Increase the applied signal until measurement receiver A indicates the current
level specified in the applicable limit is flowing in the center conductor of the
calibration fixture.
(3) Record the "forward power" to the injection probe indicated on measurement
receiver B.
(4) Scan the frequency band from 10 kHz to 200 MHz and record the forward power
needed to maintain the required current amplitude.
c. EUT Testing. Perform the following procedures on each cable bundle interfacing with
each electrical connector on the EUT including complete power cables (high sides and
returns). Also perform the procedures on power cables with the power returns and
chassis grounds (green wires) excluded from the cable bundle. For connectors which
include both interconnecting leads and power, perform the procedures on the entire

CS114
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 MIL-STD-461F

bundle, on the power leads (including returns and grounds) grouped separately, and on
the power leads grouped with the returns and grounds removed.
(1) Turn on the EUT and allow sufficient time for stabilization.
(2) Susceptibility evaluation.
(a) Set the signal generator to 10 kHz with 1 kHz pulse modulation, 50% duty
cycle.
(b) Apply the forward power level determined under 5.13.3.4b(4) to the injection
probe while monitoring the induced current.
(c) Scan the required frequency range in accordance with 4.3.10.4.1 and Table
III while maintaining the forward power level at the calibration level
determined under 5.13.3.4b(4), or the maximum current level for the
applicable limit, whichever is less stringent.
(d) Monitor the EUT for degradation of performance during testing.
(e) Whenever susceptibility is noted, determine the threshold level in accordance
with 4.3.10.4.3 and verify that it is above the applicable requirement.
(f) For EUTs with redundant cabling for safety critical reasons such as multiple
data buses, use simultaneous multi-cable injection techniques.
5.13.3.5 Data presentation.
Data presentation shall be as follows:
a. Provide amplitude versus frequency plots for the forward power levels required to
obtain the calibration level as determined in 5.13.3.4b.
b. Provide tables showing scanned frequency ranges and statements of compliance with
the requirements for the susceptibility evaluation of 5.13.3.4c(2) for each interface
connector. Provide any susceptibility thresholds that were determined, along with their
associated frequencies.

CS114
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 TABLE VI. CS114 limit curves.

LIMIT CURVE NUMBERS SHOWN IN FIGURE CS-114-1 AND LIMITS

PLATFORM ALL SHIPS

AIRCRFAFT
(ABOVE DECKS) SHIPS SHIPS (NON-
(EXTERNAL AIRCRAFT SUBMARINE
AND (METALLIC) METALLIC) GROUND SPACE
FREQUENCY OR SAFETY INTERNAL (INTERNAL)
SUBMARINES (BELOW DECKS) (BELOW DECK)
RANGE CRITICAL)
**
(EXTERNAL)*

4 kHz to N - - 77 dBμA 77 dBμA 77 dBμA 77 dBμA - -

1MHz
A 5 5 2 2 2 1 3 3
10 kHz
to N 5 3 2 2 2 1 2 3
2 MHz

73
AF 5 3 - - - - 2 3

A 5 5 5 2 4 1 4 3
MIL-STD-461F

2 MHz
to N 5 5 5 2 4 1 2 3
30 MHz
AF 5 3 - - - - 2 3
TABLE VI. CS114 limit curves.

A 5 5 5 2 2 2 4 3
30 MHz

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to N 5 5 5 2 2 2 2 3

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200 MHZ
AF 5 3 - - - - 2 3

KEY: A = Army
N = Navy * For equipment located external to the pressure hull of a submarine but within the superstructure,
AF = Air Force use SHIPS (METALLIC) (BELOW DECKS)
** For equipment located in the hanger deck of Aircraft Carriers

10 December 2007
CS114
 MIL-STD-461F

109

101
97

89

83
81
77
75

69

1G
THE APPROPRIATE LIMIT CURVE SHALL
BE DETERMINED FROM TABLE VI.

100M
CURVE #5

CURVE #4

CURVE #3

CURVE #2
CURVE #1

10M
Frequency (Hz)
1M
100k
10k
37
70 69

50 49

43
57
110

90

80

60

40
120

100

Limit Level (dBμA)

FIGURE CS114-1. CS114 calibration limits.

CS114
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 MIL-STD-461F

45
40

35
Insertion Loss (dB)

30 Maximum insertion loss

25
20
15

10
Recommended
5
minimum insertion loss
0
0.001 0.01 0.1 1 10 100 1000
Frequency (MHz)

FIGURE CS114-2. Maximum insertion loss for injection probes.

CS114
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 MIL-STD-461F

Signal
Generator

Coaxial Load Amplifier

Injection
Probe

Directional
Coupler

Measurement
Receiver
Calibration B
Fixture
Attenuator

Measurement
Receiver
A

FIGURE CS114-3. Calibration setup.

CS114
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 MIL-STD-461F

Power
Input

LISN

Injection
Probe
5 cm
Monitor
Probe
5 cm

EUT

5 cm Measurement
Monitor Receiver
Probe A
5 cm
Injection
Probe Directional
Amplifier
Coupler
Interconnecting
Cables
Measurement
Receiver Signal
Actual or Simulated Generator
B
Loads and Signals

FIGURE CS114-4. Bulk cable injection evaluation.

CS114
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 MIL-STD-461F

5.14 CS115, Conducted susceptibility, bulk cable injection, impulse excitation.

5.14.1 CS115 applicability.

This requirement is applicable to all aircraft, space, and ground system interconnecting cables,
including power cables. The requirement is also applicable for surface ship and submarine
subsystems and equipment when specified by the procuring activity.
5.14.2 CS115 limit.
The EUT shall not exhibit any malfunction, degradation of performance, or deviation from
specified indications, beyond the tolerances indicated in the individual equipment or subsystems
specification, when subjected to a pre-calibrated signal having rise and fall times, pulse width,
and amplitude as specified in Figure CS115-1 at a 30 Hz rate for one minute.
5.14.3 CS115 test procedures.
5.14.3.1 Purpose.
This test procedure is used to verify the ability of the EUT to withstand impulse signals coupled
onto EUT associated cabling.
5.14.3.2 Test equipment.
The test equipment shall be as follows:
a. Pulse generator, 50 ohm, charged line (coaxial)
b. Current injection probe
c. Drive cable, 50 ohm, 2 meters, 0.5 dB or less insertion loss at 500 MHz
d. Current probe
e. Calibration fixture: coaxial transmission line with 50 ohm characteristic impedance,
coaxial connections on both ends, and space for an injection probe around the center
conductor.
f. Oscilloscope, 50 ohm input impedance
g. Attenuators, 50 ohm
h. Coaxial loads, 50 ohm
i. LISNs
5.14.3.3 Setup.
The test setup shall be as follows:
a. Maintain a basic test setup for the EUT as shown and described in Figures 2 through 5
and 4.3.8.
b. Calibration. Configure the test equipment in accordance with Figure CS115-2 for
calibrating the injection probe.
(1) Place the injection probe around the center conductor of the calibration fixture.
(2) Terminate one end of the calibration fixture with a coaxial load and terminate the
other end with an attenuator connected to an oscilloscope with 50 ohm input
impedance.
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 MIL-STD-461F

c. EUT Testing. Configure the test equipment as shown in Figure CS115-3 for testing of
the EUT.
(1) Place the injection and monitor probes around a cable bundle interfacing with an
EUT connector.
(2) To minimize errors, maintain the same signal circuit that was used for calibration
between the attenuator at the calibration fixture (oscilloscope, coaxial cables,
bulkhead connectors, additional attenuators, etc.) and connect the circuit to the
monitor probe. Additional attenuation may be used, if necessary.
(3) Locate the monitor probe 5 cm from the connector. If the overall length of the
connector and backshell exceeds 5 cm, position the monitor probe as close to the
connector's backshell as possible.
(4) Position the injection probe 5 cm from the monitor probe.
5.14.3.4 Procedures.
The test procedures shall be as follows:
a. Turn on the measurement equipment and allow sufficient time for stabilization.
b. Calibration. Perform the following procedures using the calibration setup.
(1) Adjust the pulse generator source for the risetime, pulse width, and pulse
repetition rate requirements specified in the requirement.
(2) Increase the signal applied to the calibration fixture until the oscilloscope
indicates that the current level specified in the requirement is flowing in the
center conductor of the calibration fixture.
(3) Verify that the rise time, fall time, and pulse width portions of the waveform have
the correct durations and that the correct repetition rate is present. The precise
pulse shape will not be reproduced due to the inductive coupling mechanism.
(4) Record the pulse generator amplitude setting.
c. EUT Testing.
(1) Turn on the EUT and allow sufficient time for stabilization.
(2) Susceptibility evaluation.
(a) Adjust the pulse generator, as a minimum, for the amplitude setting
determined in 5.14.3.4b(4).
(b) Apply the test signal at the pulse repetition rate and for the duration specified
in the requirement.
(c) Monitor the EUT for degradation of performance during testing.
(d) Whenever susceptibility is noted, determine the threshold level in accordance
with 4.3.10.4.3 and verify that it is above the limit.
(e) Record the peak current induced in the cable as indicated on the oscilloscope.

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 MIL-STD-461F

(f) Repeat 5.14.3.4c(2)(a) through 5.14.3.4c(2)(e) on each cable bundle

interfacing with each electrical connector on the EUT. For power cables,
perform 5.14.3.4c(2)(a) through 5.14.3.4c(2)(e) on complete power cables
(high sides and returns) and on the power cables with the power returns and
chassis grounds (green wires) excluded from the cable bundle. For
connectors which include both interconnecting leads and power, perform
5.14.3.4c(2)(a) through 5.14.3.4c(2)(e) on the entire bundle, on the power
leads (including returns and grounds) grouped separately, and on the power
leads grouped with the returns and grounds removed.
5.14.3.5 Data presentation.
Data presentation shall be as follows:
a. Provide tables showing statements of compliance with the requirement for the
susceptibility evaluation of 5.14.3.4c(2) and the induced current level for each interface
connector.
b. Provide any susceptibility thresholds that were determined.
c. Provide oscilloscope photographs of injected waveforms with test data.

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 MIL-STD-461F

30 ns. (Minimum)
5

90%

4 REPETITION RATE = 30Hz

Limit Level (Amps)

10%

0
≤2 ≤2
Nanoseconds

FIGURE CS115-1. CS115 signal characteristics for all applications.

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 MIL-STD-461F

Coaxial Load

Drive
Injection Cable
Probe

Pulse
Generator

Calibration
Fixture
Attenuator

Oscilloscope
(50 Ω Input)

FIGURE CS115-2. Calibration setup.

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 MIL-STD-461F

Power
Input

LISN

Injection
Probe
5 cm
Monitor
Probe
5 cm

EUT

5 cm
Oscilloscope
Monitor (50 Ω Input)
Probe
5 cm
Injection
Probe Pulse
Generator
Interconnecting
Cables
Drive Cable

Actual or Simulated
Loads and Signals

FIGURE CS115-3. Bulk cable injection.

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 MIL-STD-461F

5.15 CS116, conducted susceptibility, damped sinusoidal transients, cables and power
leads, 10 kHz to 100 MHz.

5.15.1 CS116 applicability.

This requirement is applicable to all interconnecting cables, including power cables, and
individual high side power leads. Power returns and neutrals need not be tested individually.
For submarine applications, this requirement is applicable only to cables and leads that exit the
pressure hull.
5.15.2 CS116 limit.
The EUT shall not exhibit any malfunction, degradation of performance, or deviation from
specified indications, beyond the tolerances indicated in the individual equipment or subsystem
specification, when subjected to a signal having the waveform shown in Figure CS116-1 and
having a maximum current as specified in Figure CS116-2. The limit is applicable across the
entire specified frequency range. As a minimum, compliance shall be demonstrated at the
following frequencies: 0.01, 0.1, 1, 10, 30, and 100 MHz. If there are other frequencies known
to be critical to the equipment installation, such as platform resonances, compliance shall also be
demonstrated at those frequencies. The test signal repetition rate shall be no greater than one
pulse per second and no less than one pulse every two seconds. The pulses shall be applied for a
period of five minutes.
5.15.3 CS116 test procedures.

5.15.3.1 Purpose.
This test procedure is used to verify the ability of the EUT to withstand damped sinusoidal
transients coupled onto EUT associated cables and power leads.
5.15.3.2 Test equipment.
The test equipment shall be as follows:
a. Damped sinusoid transient generator, ≤ 100 ohm output impedance
b. Current injection probe
c. Oscilloscope, 50 ohm input impedance
d. Calibration fixture: Coaxial transmission line with 50 ohm characteristic impedance,
coaxial connections on both ends, and space for an injection probe around the center
conductor
e. Current probes
f. Waveform recording device
g. Attenuators, 50 ohm
h. Measurement receivers
i. Coaxial loads, 50 ohm
j. LISNs
5.15.3.3 Setup.
The test setup shall be as follows:

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 MIL-STD-461F

a. Maintain a basic test setup for the EUT as shown and described in Figures 2 through 5
and 4.3.8.
b. Calibration. Configure the test equipment in accordance with Figure CS116-3 for
verification of the waveform.
c. EUT Testing:
(1) Configure the test equipment as shown in Figure CS116-4.
(2) To minimize errors, maintain the same signal circuit that was used for calibration
between the attenuator at the calibration fixture (oscilloscope, coaxial cables,
bulkhead connectors, additional attenuators, etc.) and connect the circuit to the
monitor probe. Additional attenuation may be used, if necessary.
(3) Place the injection and monitor probes around a cable bundle interfacing an EUT
connector.
(4) Locate the monitor probe 5 cm from the connector. If the overall length of the
connector and backshell exceeds 5 cm, position the monitor probe as close to the
connector's backshell as possible.
(5) Position the injection probe 5 cm from the monitor probe.
5.15.3.4 Procedures.
The test procedures shall be as follows:
a. Turn on the measurement equipment and allow sufficient time for stabilization.
b. Calibration. Perform the following procedures using the calibration setup for waveform
verification.
(1) Set the frequency of the damped sine generator at 10 kHz.
(2) Adjust the amplitude of the signal from the damped sine generator to the level
specified in the requirement.
(3) Record the damped sine generator settings.
(4) Verify that the waveform complies with the requirements.
(5) Repeat 5.15.3.4b(2) through 5.15.3.4b(4) for each frequency specified in the
requirement and those identified in 5.15.3.4c(2).
c. EUT testing. Perform the following procedures, using the EUT test setup on each cable
bundle interfacing with each connector on the EUT including complete power cables.
Also perform tests on each individual high side power lead (individual power returns
and neutrals are not required to be tested).
(1) Turn on the EUT and measurement equipment to allow sufficient time for
stabilization.
(2) Set the damped sine generator to a test frequency.
(3) Apply the calibrated test signals to each cable or power lead of the EUT
sequentially. Reduce the signal, if necessary, to produce the required current.

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 MIL-STD-461F

For shielded cables or low impedance circuits, it may be preferable to increase the
signal gradually to limit the current. Record the peak current obtained.
(4) Monitor the EUT for degradation of performance.
(5) If susceptibility is noted, determine the threshold level in accordance with
4.3.10.4.3 and verify that it is above the specified requirements.
(6) Repeat 5.15.3.4c(2) through 5.15.3.4c(5) for each test frequency as specified in
the requirement.
5.15.3.5 Data presentation.
Data presentation shall be as follows:
a. Provide a list of the frequencies and amplitudes at which the test was conducted for
each cable and lead.
b. Provide data on any susceptibility thresholds and the associated frequencies that were
determined for each connector and power lead.
c. Provide indications of compliance with the requirements for the susceptibility
evaluation specified in 5.15.3.4c for each interface connector.
d. Provide oscilloscope photographs of injected waveforms with test data.

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 MIL-STD-461F

IP
CURRENT

TIME

1/f 2/f 3/f

NOTES: 1. Normalized waveform: e -(πf t)/Q sin(2πft)

Where:
f = Frequency (Hz)
t = Time (sec)
Q = Damping factor, 15 ±5

2. Damping factor (Q) shall be determined as follows:

π(N - 1)
Q = ln(I /I )
P N

Where:
Q = Damping factor
N = Cycle number (i.e. N = 2, 3, 4, 5,…)
IP = Peak current at 1st cycle
IN = Peak current at cycle closest to 50% decay
ln = Natural log
3. IP as specified in Figure CS116-2

FIGURE CS116-1. Typical CS116 damped sinusoidal waveform.

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 MIL-STD-461F

100
Peak current (Amperes)

10

0.1
0.01 0.1 1 10 100
Frequency (MHz)

FIGURE CS116-2. CS116 limit for all applications.

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 MIL-STD-461F

Coaxial Load

Injection
Probe

Damped Sinusoid
Transient Generator

Calibration
Fixture
Attenuator

Storage
Oscilloscope

FIGURE CS116-3. Typical test setup for calibration of test waveform.

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 MIL-STD-461F

Power
Input

LISN

Injection
Probe
5 cm
Monitor
Probe
5 cm

EUT

5 cm Storage
Monitor Oscilloscope
Probe
5 cm
Damped
Injection
Sinusoid
Probe
Generator
Interconnecting
Cables

Actual or Simulated
Loads and Signals

FIGURE CS116-4. Typical set up for bulk cable injection of damped sinusoidal transients.

CS116
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 MIL-STD-461F

5.16 RE101, radiated emissions, magnetic field, 30 Hz to 100 kHz.

5.16.1 RE101 applicability.

This requirement is applicable for radiated emissions from equipment and subsystem enclosures,
including electrical cable interfaces. The requirement does not apply to radiation from antennas.
For Navy aircraft, this requirement is applicable only for aircraft with an ASW capability.
5.16.2 RE101 limit.
Magnetic field emissions shall not be radiated in excess of the levels shown in Figures RE101-1
and RE101-2 at a distance of 7 cm.
5.16.3 RE101 test procedures.
5.16.3.1 Purpose.
This test procedure is used to verify that the magnetic field emissions from the EUT and its
associated electrical interfaces do not exceed specified requirements.
5.16.3.2 Test equipment.
The test equipment shall be as follows:
a. Measurement receivers
b. Data recording device
c. Loop sensor having the following specifications:
(1) Diameter: 13.3 cm
(2) Number of turns: 36
(3) Wire: DC resistance between 5 and 10 ohms
(4) Shielding: Electrostatic
(5) Correction factor: See manufacturer’s data for factors to convert measurement
receiver readings to decibels above one picotesla (dBpT).
d. LISNs
e. Ohmmeter
f. Signal generator
5.16.3.3 Setup.
The test setup shall be as follows:
a. Maintain a basic test setup for the EUT as shown and described in Figures 2 through 5
and 4.3.8.
b. Calibration. Configure the measurement setup as shown in Figure RE101-3.
c. EUT Testing. Configure the measurement receiving loop and EUT as shown in Figure
RE101-4.
5.16.3.4 Procedures.
The test procedures shall be as follows:

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 MIL-STD-461F

a. Turn on the measurement equipment and allow sufficient time for stabilization.
b. Calibration.
(1) Apply a calibrated signal level, which is at least 6 dB below the limit (limit minus
the loop sensor correction factor), at a frequency of 50 kHz. Tune the
measurement receiver to a center frequency of 50 kHz. Record the measured
level.
(2) Verify that the measurement receiver indicates a level within ±3 dB of the
injected signal level.
(3) If readings are obtained which deviate by more than ±3 dB, locate the source of
the error and correct the deficiency prior to proceeding with the testing.
(4) Using an ohmmeter, verify that the resistance of the loop sensor winding is
approximately 10 ohms.
c. EUT Testing.
(1) Turn on the EUT and allow sufficient time for stabilization.
(2) Locate the loop sensor 7 cm from the EUT face or electrical interface connector
being probed. Orient the plane of the loop sensor parallel to the EUT faces and
parallel to the axis of connectors.
(3) Scan the measurement receiver over the applicable frequency range to locate the
frequencies of maximum radiation, using the bandwidths and minimum
measurement times of Table II.
(4) Tune the measurement receiver to one of the frequencies or band of frequencies
identified in 5.16.3.4c(3) above.
(5) Monitor the output of the measurement receiver while moving the loop sensor
(maintaining the 7 cm spacing) over the face of the EUT or around the connector.
Note the point of maximum radiation for each frequency identified in
5.16.3.4c(4).
(6) At 7 cm from the point of maximum radiation, orient the plane of the loop sensor
to give a maximum reading on the measurement receiver and record the reading.
If the measured emission exceeds the limit at the 7 cm distance, increase the
measurement distance until the emission falls within the specified limit. Record
the emissions and the measurement distance for assessment by the procuring
activity. NOTE: The EUT shall comply with the applicable RE101 limit at 7 cm.
(7) Repeat 5.16.3.4c(4) through 5.16.3.4c(6) for at least two frequencies of maximum
radiation per octave of frequencies below 200 Hz and for at least three
frequencies of maximum radiation per octave above 200 Hz.
(8) Repeat 5.16.3.4c(2) through 5.16.3.4c(7) for each face of the EUT and for each
EUT electrical connector.

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 MIL-STD-461F

5.16.3.5 Data presentation.

Data presentation shall be as follows:
a. Provide graphs of scans and tabular listings of each measurement frequency, mode of
operation, measured magnetic field, and magnetic field limit level.

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 MIL-STD-461F

190

180

170

160
Limit Level (dBpT)

150

140

130

120

110

100
10 100 1k 10k 100k 1M
Frequency (Hz)

FIGURE RE101-1. RE101 limit for all Army applications.

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 MIL-STD-461F

170

160

150

140

130
Limit Level (dBpT)

120
114
110

100

90

80
76
70

60 450
10 100 1k 10k 100k
Frequency (Hz)

FIGURE RE101-2. RE101 limit for all Navy applications.

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 MIL-STD-461F

Coaxial
Measurement Cable Signal
Receiver Generator

FIGURE RE101-3. Calibration configuration.

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 MIL-STD-461F

Power
Input

LISN

7 cm
Receiving
Loop

Measurement EUT
Receiver

FIGURE RE101-4. Basic test setup.

RE101
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 MIL-STD-461F

5.17 RE102, radiated emissions, electric field, 10 kHz to 18 GHz.

5.17.1 RE102 applicability.

This requirement is applicable for radiated emissions from equipment and subsystem enclosures,
all interconnecting cables, and antennas designed to be permanently mounted to EUTs (receivers
and transmitters in standby mode). The requirement does not apply at the transmitter
fundamental frequencies and the necessary occupied bandwidth of the signal. The requirement
is applicable as follows:
a. Ground 2 MHz to 18 GHz*
b. Ships, surface 10 kHz to 18 GHz*
c. Submarines 10 kHz to 18 GHz*
d. Aircraft (Army and Navy ASW) 10 kHz to 18 GHz
e. Aircraft (Air Force and Navy) 2 MHz to 18 GHz*
f. Space 10 kHz to 18 GHz*
*Testing is required up to 1 GHz or 10 times the highest intentionally generated frequency
within the EUT, whichever is greater. Measurements beyond 18 GHz are not required.
5.17.2 RE102 limits.
Electric field emissions shall not be radiated in excess of those shown in Figures RE102-1
through RE102-4. Above 30 MHz, the limits shall be met for both horizontally and vertically
polarized fields.
5.17.3 RE102 test procedures.

5.17.3.1 Purpose.
This test procedure is used to verify that electric field emissions from the EUT and its associated
cabling do not exceed specified requirements.
5.17.3.2 Test equipment.
The test equipment shall be as follows:
a. Measurement receivers
b. Data recording device
c. Antennas
(1) 10 kHz to 30 MHz, 104 cm rod with impedance matching network. The signal
output connector shall be bonded to the antenna matching network case.
(a) When the impedance matching network includes a preamplifier (active rod),
observe the overload precautions in 4.3.7.3.
(b) Use a square counterpoise measuring at least 60 cm on a side.
(2) 30 MHz to 200 MHz, Biconical, 137 cm tip to tip.
(3) 200 MHz to 1 GHz, Double ridge horn, 69.0 by 94.5 cm opening.
(4) 1 GHz to 18 GHz, Double ridge horn, 24.2 by 13.6 cm opening

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 MIL-STD-461F

d. Signal generators
e. Stub radiator
f. Capacitor, 10 pF
g. LISNs
5.17.3.3 Setup.
The test setup shall be as follows:
a. Maintain a basic test setup for the EUT as shown and described in Figures 1 through 5
and 4.3.8. Ensure that the EUT is oriented such that the surface that produces the
maximum radiated emissions is toward the front edge of the test setup boundary.
b. Calibration. Configure the test equipment as shown in Figure RE102-5.
c. EUT testing.
(1) For rod antenna measurements, electrical bonding of the counterpoise is
prohibited. The required configuration is shown in Figure RE102-6. The shield of
the coaxial cable from the rod antenna matching network shall be electrically
bonded to the floor in a length as short as possible (not to exceed 10 cm excess
length). A ferrite sleeve with 20 to 30 ohms impedance at 20 MHz shall be
placed near the center of the coaxial cable length between the antenna matching
network and the floor.
(2) Antenna Positioning.
(a) Determine the test setup boundary of the EUT and associated cabling for use
in positioning of antennas.
(b) Use the physical reference points on the antennas shown in Figure RE102-6
for measuring heights of the antennas and distances of the antennas from the
test setup boundary.
1. Position antennas 1 meter from the front edge of the test setup boundary
for all setups.
2. Position antennas 120 cm above the floor ground plane.
3. Ensure that no part of any antenna is closer than 1 meter from the walls
and 0.5 meter from the ceiling of the shielded enclosure.
(c) The number of required antenna positions depends on the size of the test
setup boundary and the number of enclosures included in the setup.
1. For testing below 200 MHz, use the following criteria to determine the
individual antenna positions.
a. For setups with the side edges of the boundary 3 meters or less, one
position is required and the antenna shall be centered with respect to
the side edges of the boundary.
b. For setups with the side edges of the boundary greater than 3 meters,
use multiple antenna positions at spacings as shown in

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 MIL-STD-461F

Figure RE102-7. Determine the number of antenna positions (N) by

dividing the edge-to-edge boundary distance (in meters) by 3 and
rounding up to an integer.
2. For testing from 200 MHz up to 1 GHz, place the antenna in a sufficient
number of positions such that the entire width of each EUT enclosure
and the first 35 cm of cables and leads interfacing with the EUT
enclosure are within the 3 dB beamwidth of the antenna.
3. For testing at 1 GHz and above, place the antenna in a sufficient number
of positions such that the entire width of each EUT enclosure and the
first 7 cm of cables and leads interfacing with the EUT enclosure are
within the 3 dB beamwidth of the antenna.
5.17.3.4 Procedures.
The test procedures shall be as follows:
a. Verify that the ambient requirements specified in 4.3.4 are met. Take plots of the
ambient when required by the referenced paragraph.
b. Turn on the measurement equipment and allow a sufficient time for stabilization.
c. Using the system check path of Figure RE102-5, perform the following evaluation of
the overall measurement system from each antenna to the data output device at the
highest measurement frequency of the antenna. For rod antennas that use passive
matching networks, the evaluation shall be performed at the center frequency of each
band. For active rod antennas, the evaluation shall be performed at the lowest
frequency of test, at a mid-band frequency, and at the highest frequency of test.
(1) Apply a calibrated signal level, which is at least 6 dB below the limit (limit minus
antenna factor), to the coaxial cable at the antenna connection point.
(2) Scan the measurement receiver in the same manner as a normal data scan. Verify
that the data recording device indicates a level within ±3 dB of the injected signal
level.
(3) For the 104 cm rod antenna, remove the rod element and apply the signal to the
antenna matching network through a 10 pF capacitor connected to the rod mount
as shown in Figure RE102-8. Commercial calibration jigs or injection networks
shall not be used.
(4) If readings are obtained which deviate by more than ±3 dB, locate the source of
the error and correct the deficiency prior to proceeding with the testing.
d. Using the measurement path of Figure RE102-5, perform the following evaluation for
each antenna to demonstrate that there is electrical continuity through the antenna.
(1) Radiate a signal using an antenna or stub radiator at the highest measurement
frequency of each antenna.
(2) Tune the measurement receiver to the frequency of the applied signal and verify
that a received signal of appropriate amplitude is present. Note: This evaluation

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 MIL-STD-461F

is intended to provide a coarse indication that the antenna is functioning properly.

There is no requirement to accurately measure the signal level.
e. Turn on the EUT and allow sufficient time for stabilization.
f. Using the measurement path of Figure RE102-5, determine the radiated emissions from
the EUT and its associated cabling.
(1) Scan the measurement receiver for each applicable frequency range, using the
bandwidths and minimum measurement times in Table II.
(2) Above 30 MHz, orient the antennas for both horizontally and vertically polarized
fields.
(3) Take measurements for each antenna position determined under 5.17.3.3c(2)(c)
above.
5.17.3.5 Data presentation.
Data presentation shall be as follows:
a. Continuously and automatically plot amplitude versus frequency profiles. Manually
gathered data is not acceptable except for plot verification. Vertical and horizontal data
for a particular frequency range shall be presented on separate plots or shall be clearly
distinguishable in black or white format for a common plot.
b. Display the applicable limit on each plot.
c. Provide a minimum frequency resolution of 1% or twice the measurement receiver
bandwidth, whichever is less stringent, and a minimum amplitude resolution of 1 dB for
each plot.
d. Provide plots for both the measurement and system check portions of the procedure.
e. Provide a statement verifying the electrical continuity of the measurement antennas as
determined in 5.17.3.4d.

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 MIL-STD-461F

110
102
100

90
Limit Level (dBμV/m)

82
80 Below Deck

70

60
56
50
Topside
40
36

30 18G
10k 100k 1M 10M 100M 1G 10G 100G
Frequency (Hz)

FIGURE RE102-1. RE102 limit for surface ship applications.

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 MIL-STD-461F

100
95
90

80

70 69
Limit Level (dBμV/m)

60 Internal to
Pressure Hull
50

40

30 External to
Pressure Hull
24
20

10 18G
10k 100k 1M 10M 100M 1G 10G 100G
Frequency (Hz)

FIGURE RE102-2. RE102 limit for submarine applications.

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 MIL-STD-461F

90 89

80 79

70 69

60
Limit Level (dBμV/m)

Fixed Wing Internal,

50 >25 meters Nose to Tail

44
40 Fixed Wing Internal,
< 25 meters Nose to Tail
34
30
24
20
Fixed Wing External (2MHz to18 GHz)
and Helicopters
10
18G
10k 100k 1M 10M 100M 1G 10G 100G
Frequency (Hz)

FIGURE RE102-3. RE102 limit for aircraft and space system applications.

RE102
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 MIL-STD-461F

100

90 89

80

70 69
Limit Level (dBμV/m)

60
Navy Fixed & Air Force
50
44
40

Navy Mobile & Army

30
24
20

10 18G
100k 1M 10M 100M 1G 10G 100G
Frequency (Hz)

FIGURE RE102-4. RE102 limit for ground applications.

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 MIL-STD-461F

TEST SETUP BOUNDARY

Antenna

Path for
Measurement

Signal
Generator

Path for
System Check
Shielded Enclosure

Coaxial
Cable

Measurement
Receiver

Data
Recording
Device

FIGURE RE102-5. Basic test setup.

RE102
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 MIL-STD-461F

Center Point of Rod

Element

Test Setup Note: No Bond Strap

Boundary

ROD

120 cm
80-90 cm

Ground Plane Coaxial Cable Shield Ferrite, 20 - 30

Bonded to Floor Using Ohms @ 20 MHz
Elbow Adaptor and
Clamp Floor

Test Setup
Boundary

BICONICAL
120 cm
80-90 cm

Ground
Plane
Floor

Test Setup
Boundary

DOUBLE
RIDGE HORN
120 cm
80-90 cm

Ground
Plane

Floor

1m

FIGURE RE102-6. Antenna positioning.

RE102
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 MIL-STD-461F

1m

LISN
2N
X

1m
Loads
To
N
X
TEST SETUP BOUNDARY
Rounded Up to an Integer

1m
N=2

2m
2m
Positions
Antenna

EXAMPLE: X = 4 m

2m
X

EUT
X (in meters)
3

Platform
Length
Actual

<2m
N=

1m
N
X

EUT
2N
X

FIGURE RE102-7. Multiple antenna positions.

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 MIL-STD-461F

Counterpoise

Coaxial Cable From Center Conductors

Signal Source Tied Together and
to 10 pF Capacitor
10 pF Capacitor
Rod Tied to Rod
Matching Connection
Network

Shields tied Coaxial Cable

Together and to to Measurement
Network Case Receiver

Coaxial Cable
to Termination
50 Ohm RF
Termination

Notes:
1. Each individual wire connection limited to 5 cm length maximum.
2. 50 ohm termination may be replaced with 50 ohm measurement
receiver to verify level of injected signal.
3. The 10 pF capacitor may be built into some antenna matching
networks.

FIGURE RE102-8. Rod antenna system check.

RE102
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 MIL-STD-461F

5.18 RE103, radiated emissions, antenna spurious and harmonic outputs, 10 kHz to 40
GHz.

5.18.1 RE103 applicability.

This requirement may be used as an alternative for CE106 when testing transmitters with their
intended antennas. This requirement is met if the emissions do not exceed the applicable RE102
limit. CE106 is the preferred requirement unless the equipment or subsystem design
characteristics preclude its use. The requirement is not applicable within the bandwidth of the
EUT transmitted signal or within ±5 percent of the fundamental frequency, whichever is larger.
Depending on the operating frequency range of the EUT, the start frequency of the test is as
follows:
Operating Frequency Range (EUT) Start Frequency of Test
10 kHz to 3 MHz 10 kHz
3 MHz to 300 MHz 100 kHz
300 MHz to 3 GHz 1 MHz
3 GHz to 40 GHz 10 MHz
The end frequency of the test is 40 GHz or twenty times the highest generated frequency within
the EUT, whichever is less. For equipment using waveguide, the requirement does not apply
below eight-tenths of the waveguide's cutoff frequency.
5.18.2 RE103 limits.
Harmonics, except the second and third, and all other spurious emissions shall be at least 80 dB
down from the level at the fundamental. The second and third harmonics shall be suppressed to
a level of -20 dBm or 80 dB below the fundamental, whichever requires less suppression.
5.18.3 RE103 test procedures.

5.18.3.1 Purpose.
This test procedure is used to verify that radiated spurious and harmonic emissions from
transmitters do not exceed the specified requirements.
5.18.3.2 Test equipment.
The test equipment shall be as follows:
a. Measurement receiver
b. Attenuators, 50 ohm
c. Antennas
d. Rejection networks
e. Signal generators
f. Power monitor
5.18.3.3 Setup.
It is not necessary to maintain the basic test setup for the EUT as shown and described in
Figures 1 through 5 and 4.3.8. The test setup shall be as follows:

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 MIL-STD-461F

a. Calibration. Configure the test setup for the signal check path shown in Figure
RE103-1 or RE103-2 as applicable.
b. EUT Testing. Configure the test setup for the measurement path shown in Figure
RE103-1 or RE103-2 as applicable.
5.18.3.4 Procedures.
The test procedures shall be as follows:
a. The measurements must be performed in the far-field of the transmitting frequency.
Consequently, the far-field test distance must be calculated prior to performing the test
using the relationships below:
R = distance between transmitter antenna and receiver antenna.
D = maximum physical dimension of transmitter antenna.
d = maximum physical dimension of receiver antenna.
λ = wavelength of frequency of the transmitter.
All dimensions are in meters.
For transmitter frequencies less than or equal to 1.24 GHz, the greater distance of the
following relationships shall be used:
R = 2D2/λ R = 3λ
For transmitter frequencies greater than 1.24 GHz, the separation distance shall be
calculated as follows:
For 2.5 D < d use R = 2D2/λ
For 2.5 D ≥ d use R = (D+d)2/λ
b. Turn on the measurement equipment and allow sufficient time for stabilization.
c. Calibration.
(1) Apply a known calibrated signal level from the signal generator through the
system check path at a midband fundamental frequency (fo).
(2) Scan the measurement receiver in the same manner as a normal data scan. Verify
the measurement receiver detects a level within ±3 dB of the expected signal.
(3) If readings are obtained which deviate by more than ±3 dB, locate the source of
the error and correct the deficiency prior to proceeding with the test.
(4) Repeat 5.18.3.4c(1) through 5.18.3.4c(3) for two other frequencies over the
frequency range of test.
d. EUT Testing.
(1) Turn on the EUT and allow a sufficient time for stabilization.
(2) Tune the EUT to the desired test frequency and use the measurement path to
complete the rest of this procedure.

RE103
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 MIL-STD-461F

(3) Tune the test equipment to the measurement frequency (fo) of the EUT and adjust
for maximum indication.
(4) For transmitters where a power monitor can be inserted, measure the modulated
transmitter power output P, using a power monitor while keying the transmitter.
Convert this power level to units of dB relative to 1 watt (dBW). Calculate the
Effective Radiated Power (ERP) by adding the EUT antenna gain to this value.
Record the resulting level for comparison with that obtained in 5.18.3.4d(6).
(5) Key the transmitter with desired modulation. Tune the measurement receiver for
maximum output indication at the transmitted frequency. If either or both of the
antennas have directivity, align both in elevation and azimuth for maximum
indication. Verbal communication between sites via radiotelephone will facilitate
this process. Record the resulting maximum receiver meter reading and the
measurement receiver bandwidth.
(6) Calculate the transmitter ERP in dBW, based on the receiver meter reading V,
using the following equation:
ERP = V + 20 log R + AF - 135
where:
V = reading on the measurement receiver in dBμV
R = distance between transmitter and receiver antennas in meters
AF = antenna factor of receiver antenna in dB (1/m)
Compare this calculated level to the measured level recorded in 5.18.3.4d(4). The
compared results should agree within ±3 dB. If the difference exceeds ±3 dB,
check the test setup for errors in measurement distance, amplitude calibration,
power monitoring of the transmitter, frequency tuning or drift and antenna
boresight alignment. Assuming that the results are within the ±3 dB tolerance,
the ERP becomes the reference for which amplitudes of spurious and harmonics
will be compared to determine compliance with standard limits.
(7) With the rejection network filter connected and tuned to fo, scan the measurement
receiver over the frequency range of test to locate spurious and harmonic
transmitted outputs. It may be necessary to move the measuring system antenna
in elevation and azimuth at each spurious and harmonic output to assure
maximum levels are recorded. Maintain the same measurement receiver
bandwidth used to measure the fundamental frequency in 5.18.3.4d(5).
(8) Verify that spurious outputs are from the EUT and not spurious responses of the
measurement system or the test site ambient.
(9) Calculate the ERP of each spurious output. Include all correction factors for
cable loss, amplifier gains, filter loss, and attenuator factors.
(10) Repeat 5.18.3.4d(2) through 5.18.3.4d(9) for other fo of the EUT.

RE103
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 MIL-STD-461F

5.18.3.5 Data presentation.

Data presentation shall be as follows:
a. Provide tabular data showing fundamental frequency (fo) and frequency of all
harmonics and spurious emissions measured, the measured power monitor level and the
calculated ERP of the fundamental frequency, the ERP of all spurious and harmonics
emissions measured, dB down levels, and all correction factors including cable loss,
attenuator pads, amplifier gains, insertion loss of rejection networks and antenna gains.
The relative dB down level is determined by subtracting the level in 5.18.3.4d(6) from
that recorded in 5.18.3.4d(9).

RE103
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 MIL-STD-461F

TX Antenna RX Antenna
Path for Measurement

Path for Band Rejection

System or
Check High Pass Filter
Transmitter
EUT

Signal
Generator

Power
Monitor

Attenuator

Measurement
Receiver

FIGURE RE103-1. Calibration and test setup for radiated harmonics and spurious
emissions, 10 kHz to 1 GHz.

RE103
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 MIL-STD-461F

TX Antenna Path for Measurement RX Antenna

Path for Band Rejection

System or
Check High Pass Filter
Transmitter
EUT

Signal
Generator
Power
Monitor
Preselector
or Filter

Variable
Attenuator

Measurement
Receiver

FIGURE RE103-2. Calibration and test setup for radiated harmonics and spurious
emissions, 1 GHz to 40 GHz.

RE103
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 MIL-STD-461F

5.19 RS101, radiated susceptibility, magnetic field, 30 Hz to 100 kHz.

5.19.1 RS101 applicability.

This requirement is applicable to equipment and subsystem enclosures, including electrical cable
interfaces. The requirement is not applicable for electromagnetic coupling via antennas. For
equipment intended to be installed on Navy aircraft, the requirement is applicable only to aircraft
with ASW capability. For Army ground equipment, the requirement is applicable only to
vehicles having a minesweeping or mine detection capability. For submarines, this requirement
is applicable only to equipment and subsystems that have an operating frequency of 100 kHz or
less and an operating sensitivity of 1 μV or better (such as 0.5 μV).
5.19.2 RS101 limit.
The EUT shall not exhibit any malfunction, degradation of performance, or deviation from
specified indications, beyond the tolerances indicated in the individual equipment or subsystem
specification, when subjected to the magnetic fields shown in Figures RS101-1 and RS101-2.
5.19.3 RS101 test procedures.

5.19.3.1 Purpose.
This test procedure is used to verify the ability of the EUT to withstand radiated magnetic fields.
5.19.3.2 Test equipment.
The test equipment shall be as follows:
a. Signal source
b. Radiating loop having the following specifications:
(1) Diameter: 12 cm
(2) Number of turns: 20
(3) Wire: No. 12 insulated copper
(4) Magnetic flux density: 9.5x107 pT/ampere of applied current at a distance of
5 cm from the plane of the loop.
c. Loop sensor having the following specifications:
(1) Diameter: 4 cm
(2) Number of turns: 51
(3) Wire: 7-41 Litz wire (7 Strand, No. 41 AWG)
(4) Shielding: Electrostatic
(5) Correction Factor: See manufacturer’s data for factors to convert measurement
receiver readings to decibels above one picotesla (dBpT).
d Measurement receiver or narrowband voltmeter
e. Current probe
f. LISNs
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 MIL-STD-461F

5.19.3.3 Setup.
The test setup shall be as follows:
a. Maintain a basic test setup for the EUT as shown and described in Figures 2 through 5
and 4.3.8.
b. Calibration. Configure the measurement equipment, radiating loop, and loop sensor as
shown in Figure RS101-3.
c. EUT Testing. Configure the test as shown in Figure RS101-4.
5.19.3.4 Procedures.
The test procedures shall be as follows:
a. Turn on the measurement equipment and allow sufficient time for stabilization.
b. Calibration.
(1) Set the signal source to a frequency of 1 kHz and adjust the output to provide a
magnetic flux density of 110 dB above one picotesla as determined by the reading
obtained on measurement receiver A and the relationship given in 5.19.3.2b(4).
(2) Measure the voltage output from the loop sensor using measurement receiver B.
(3) Verify that the output on measurement receiver B is within ±3 dB of the expected
value based on the antenna factor and record this value.
c. EUT Testing.
(1) Turn on the EUT and allow sufficient time for stabilization.
(2) Select test frequencies as follows:
(a) Locate the loop sensor 5 cm from the EUT face or electrical interface
connector being probed. Orient the plane of the loop sensor parallel to the
EUT faces and parallel to the axis of connectors.
(b) Supply the loop with sufficient current to produce magnetic field strengths at
least 10 dB greater than the applicable limit but not to exceed 15 amps (183
dBpT).
(c) Scan the applicable frequency range using the scan rates in Table III.
(d) If susceptibility is noted, select no less than three test frequencies per octave
at those frequencies where the maximum indications of susceptibility are
present.
(e) Reposition the loop successively to a location in each 30 by 30 cm area on
each face of the EUT and at each electrical interface connector, and repeat
5.19.3.4c(2)(c) and 5.19.3.4c(2)(d) to determine locations and frequencies of
susceptibility.
(f) From the total frequency data where susceptibility was noted in
5.19.3.4c(2)(c) through 5.19.3.4c(2)(e), select three frequencies per octave
over the applicable frequency range.
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 MIL-STD-461F

(3) At each frequency determined in 5.19.3.4c(2)(f), apply a current to the radiating

loop that corresponds to the applicable limit. Move the loop to search for
possible locations of susceptibility with particular attention given to the locations
determined in 5.19.3.4c(2)(e) while maintaining the loop 5 cm from the EUT
surface or connector. Verify that susceptibility is not present.
5.19.3.5 Data presentation.
Data presentation shall be as follows:
a. Provide tabular data showing verification of the calibration of the radiating loop in
5.19.3.4b.
b. Provide tabular data, diagrams, or photographs showing the applicable test frequencies
and locations determined in 5.19.3.4c(2)(e) and 5.19.3.4c(2)(f).
c. Provide graphical or tabular data showing frequencies and threshold levels of
susceptibility.
5.19.4 RS101 alternative test procedures – AC Helmholtz coil.
This test procedure may be substituted for the 5.19.3 procedures, provided that the EUT size
versus coil size constraints of 5.19.4.3b can be satisfied.
5.19.4.1 Purpose.
This test procedure is an alternative technique used to verify the ability of the EUT to withstand
radiated magnetic fields.
5.19.4.2 Test equipment.
The test equipment shall be as follows:
a. Signal source
b. Series-wound AC Helmholtz coil
c. Loop sensor having the following specifications (same as RE101 loop):
(1) Diameter: 13.3 cm
(2) Number of turns: 36
(3) Wire: DC resistance between 5 and 10 ohms
(4) Shielding: Electrostatic
(5) Correction factor: See manufacturer’s data for factors to convert measurement
receiver readings to decibels above one picotesla (dBpT).
d Measurement receiver or narrowband voltmeter
e. Current probe
f. LISNs
5.19.4.3 Setup.
The test setup shall be as follows:

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 MIL-STD-461F

a. Maintain a basic test setup for the EUT as shown and described in Figures 2 through 5
and 4.3.8.
b. Calibration.
(1) Configure the radiating system as shown in Figure RS101-5. Select coil spacing
based on the physical dimensions of the EUT enclosure.
(2) For an EUT with dimensions less than one coil radius, use a standard Helmholtz
configuration (coils separated by one coil radius). Place the field monitoring loop
in the center of the test volume.
(3) For an EUT with dimensions greater than one coil radius, use the optional
configuration. Select a coil separation such that the plane of the EUT face is at
least 5 cm from the plane of the coils and such that the separation between the
coils does not exceed 1.5 radii. Place the field monitoring probe in the plane of
either coil at its center.
c. EUT Testing.
(1) Configure the test as shown in Figure RS101-6, using the same coil spacing
arrangement as determined for calibration under 5.19.4.3b.
(2) Position the coils such that the plane of the EUT faces is in parallel with the plane
of the coils.
5.19.4.4 Procedures.
The test procedures shall be as follows:
a. Turn on the measurement equipment and allow sufficient time for stabilization.
b. Calibration.
(1) Set the signal source to a frequency of 1 kHz and adjust the output current to
generate a magnetic flux density of 110 dB above one picotesla as determined by
the reading obtained on measurement receiver A.
(2) Measure the voltage output from the loop sensor using measurement receiver B.
(3) Verify that the output on measurement receiver B is within ±3 dB of the expected
value based on the antenna factor and record this value.
c. EUT Testing.
(1) Turn on the EUT and allow sufficient time for stabilization.
(2) Select test frequencies as follows:
(a) Supply the Helmholtz coil with sufficient current to produce magnetic field
strengths at least 6 dB greater than the applicable limit.
(b) Scan the applicable frequency range using the scan rates in Table III.

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 MIL-STD-461F

(c) If susceptibility is noted, select no less than three test frequencies per octave
at those frequencies where the maximum indications of susceptibility are
present.
(d) Reposition the Helmholtz coils successively over all areas on each face of the
EUT (in all three axes), including exposure of any electrical interface
connectors, and repeat 5.19.4.4c(2)(b) and 5.19.4.4c(2)(c) to determine
locations and frequencies of susceptibility.
(e) From the total frequency data where susceptibility was noted in
5.19.4.4c(2)(b) through 5.19.4.4c(2)(d), select three frequencies per octave
over the applicable frequency range.
(3) At each frequency determined in 5.19.4.4c(2)(e), apply a current to the Helmholtz
coil that corresponds to the applicable RS101 limit. Move the coils to search for
possible locations of susceptibility with particular attention given to the locations
determined in 5.19.4.4c(2)(d). Ensure the EUT remains centered between the
coils, or the coils remain 5 cm from the EUT surface, as applicable. Verify that
susceptibility is not present.
5.19.4.5 Data presentation.
Data presentation shall be as follows:
a. Provide tabular data showing verification of the calibration of the Helmholtz coils in
5.19.4.4b.
b. Provide tabular data, diagrams, or photographs showing the applicable test frequencies
and locations determined in 5.19.4.4c(2)(d) and 5.19.4.4c(2)(e).
c. Provide graphical or tabular data showing frequencies and threshold levels of
susceptibility.

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 MIL-STD-461F

180

170

160

150
Limit Level (dBpT)

140

130

120
117

110

100
10 100 1k 10k 100k
Frequency (Hz)

FIGURE RS101-1. RS101 limit for all Navy applications.

RS101
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 MIL-STD-461F

190

180

170

160
Limit Level ( dBpT )

150

140

130

120
116

110

100
10 100 1k 10k 100k
Frequency (Hz)

FIGURE RS101-2. RS101 limit for all Army applications.

RS101
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 MIL-STD-461F

5c
m

Radiating
Loop

Signal
Source
Current
Probe

Field
Monitoring
Loop

Measurement
Receiver A

Measurement
Receiver B

FIGURE RS101-3. Calibration of the radiating system.

RS101
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 MIL-STD-461F

Power
Input

LISN

5 cm

Radiating
Loop

Signal
EUT
Source

Current
Probe

Measurement
Receiver

Actual and
Simulated Loads
and Signals

FIGURE RS101-4. Basic test setup.

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 MIL-STD-461F

Radiating Loop A Se
par
atio
n=
Measurement r r
2
Receiver A Measurement
Receiver B
Current Probe
r

r
Signal
Source

Field Monitoring Loop

Radiating Loop B

Standard Configuration

r<
Se
Radiating Loop A par
atio
n <1
Measurement .5 r
Receiver A Measurement
Receiver B
Current Probe
r

r
Signal
Source Field Monitoring Loop

Radiating Loop B

Optional Configuration

FIGURE RS101-5. Calibration of Helmholtz coils.

RS101
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 MIL-STD-461F

LISNs
Actual or Simulated
Measurement Loads and Signals
Receiver A
Radiating
Loop B
Radiating Loop A 5 cm Minimum
Current Probe for Optional
Configuration

Signal EUT
Source

Note: One axis position of three required is shown

FIGURE RS101-6. Test setup for Helmholtz coils.

RS101
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 MIL-STD-461F

5.20 RS103, radiated susceptibility, electric field, 2 MHz to 40 GHz.

5.20.1 RS103 applicability.

This requirement is applicable to equipment and subsystem enclosures and all interconnecting
cables. The requirement is applicable as follows:
a. 2 MHz to 30 MHz Army ships; Army aircraft, including flight line; Navy
(except aircraft); and optional* for all others
b. 30 MHz to 100 MHz all (except Navy aircraft)
c. 100 MHz to 1 GHz all
d. 1 GHz to 18 GHz all
e. 18 GHz to 40 GHz optional* for all
*Required only if specified in the procurement specification
There is no requirement at the tuned frequency of antenna-connected receivers except for surface
ships and submarines.
5.20.2 RS103 limit.
The EUT shall not exhibit any malfunction, degradation of performance, or deviation from
specified indications, beyond the tolerances indicated in the individual equipment or subsystem
specification, when subjected to the radiated electric fields listed in Table VII and modulated as
specified below. Up to 30 MHz, the requirement shall be met for vertically polarized fields.
Above 30 MHz, the requirement shall be met for both horizontally and vertically polarized
fields. Circular polarized fields are not acceptable.
5.20.3 RS103 test procedures.

5.20.3.1 Purpose.
This test procedure is used to verify the ability of the EUT and associated cabling to withstand
electric fields.
5.20.3.2 Test equipment.
The test equipment shall be as follows:
a. Signal generators
b. Power amplifiers
c. Receive antennas
(1) 1 GHz to 10 GHz, double ridge horns
(2) 10 GHz to 40 GHz, other antennas as approved by the procuring activity
d. Transmit antennas
e. Electric field sensors (physically small - electrically short)
f. Measurement receiver
g. Power meter

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 MIL-STD-461F

h. Directional coupler
i. Attenuator
j. Data recording device
k. LISNs
5.20.3.3 Setup.
The test setup shall be as follows:
a. Maintain a basic test setup for the EUT as shown and described in Figures 1 through 5
and 4.3.8.
b. For electric field calibration, electric field sensors are required from 2 MHz to 1 GHz.
Either field sensors or receive antennas may be used above 1 GHz (see 5.20.3.2c and
5.20.3.2e).
c. Configure test equipment as shown in Figure RS103-1.
d. Calibration.
(1) Placement of electric field sensors (see 5.20.3.3b). Position sensors at same
distance as the EUT is located from the transmit antenna, directly opposite the
transmit antenna as shown in Figures RS103-2 and RS103-3, and a minimum of
30 cm above the ground plane at or below 1 GHz. Above 1 GHz, place the
sensors at height corresponding to the area of the EUT being illuminated. Do not
place sensors directly at corners or edges of EUT components.
(2) Placement of receive antennas (see 5.20.3.3b). Prior to placement of the EUT,
position the receive antenna, as shown in Figure RS103-4, on a dielectric stand at
the position and height above the ground plane where the center of the EUT will
be located.
e. EUT testing.
(1) Placement of transmit antennas. Antennas shall be placed 1 meter or greater from
the test setup boundary as follows:
(a) 2 MHz to 200 MHz
1 Test setup boundaries ≤ 3 meters. Center the antenna between the edges
of the test setup boundary. The boundary includes all enclosures of the
EUT and the 2 meters of exposed interconnecting and power leads
required in 4.3.8.6. Interconnecting leads shorter than 2 meters are
acceptable when they represent the actual platform installation.
2 Test setup boundaries > 3 meters. Use multiple antenna positions (N) at
spacings as shown in Figure RS103-3. The number of antenna positions
(N) shall be determined by dividing the edge-to-edge boundary distance
(in meters) by 3 and rounding up to an integer.
(b) 200 MHz and above. Multiple antenna positions may be required as shown
in Figure RS103-2. Determine the number of antenna positions (N) as
follows:

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 MIL-STD-461F

1 For testing from 200 MHz up to 1 GHz, place the antenna in a sufficient
number of positions such that the entire width of each EUT enclosure
and the first 35 cm of cables and leads interfacing with the EUT
enclosure are within the 3 dB beamwidth of the antenna.
2 For testing at 1 GHz and above, place the antenna in a sufficient number
of positions such that the entire width of each EUT enclosure and the
first 7 cm of cables and leads interfacing with the EUT enclosure are
within the 3 dB beamwidth of the antenna.
(2) Maintain the placement of electric field sensors as specified in 5.20.3.3d(1)
above.
5.20.3.4 Procedures.
The test procedures shall be as follows:
a. Turn on the measurement equipment and EUT and allow a sufficient time for
stabilization.
b. Assess the test area for potential RF hazards and take necessary precautionary steps to
assure safety of test personnel.
c. Calibration.
(1) Electric field sensor procedure. Record the amplitude shown on the electric field
sensor display unit due to EUT ambient. Reposition the sensor, as necessary,
until this level is < 10% of the applicable field strength to be used for testing.
(2) Receive antenna procedure (> 1 GHz).
(a) Connect a signal generator to the coaxial cable at the receive antenna
connection point (antenna removed). Set the signal source to an output level
of 0 dBm at the highest frequency to be used in the present test setup. Tune
the measurement receiver to the frequency of the signal source.
(b) Verify that the output indication is within ±3 dB of the applied signal,
considering all appropriate losses. If larger deviations are found, locate the
source of the error and correct the deficiency before proceeding.
(c) Connect the receive antenna to the coaxial cable as shown in Figure
RS103-4. Set the signal source to 1 kHz pulse modulation, 50% duty cycle.
Using an appropriate transmit antenna and amplifier, establish an electric
field at the test start frequency. Gradually increase the electric field level
until it reaches the applicable limit.
(d) Scan the test frequency range and record the required input power levels to
the transmit antenna to maintain the required field.
(e) Repeat procedures 5.20.3.4c(2)(a) through 5.20.3.4c(2)(d) whenever the test
setup is modified or an antenna is changed.
d. EUT Testing.
(1) E-Field sensor procedure.

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 MIL-STD-461F

(a) Set the signal source to 1 kHz pulse modulation, 50% duty cycle, and using
appropriate amplifier and transmit antenna, establish an electric field at the
test start frequency. Gradually increase the electric field level until it reaches
the applicable limit.
(b) Scan the required frequency ranges in accordance with the rates and
durations specified in Table III. Maintain field strength levels in accordance
with the applicable limit. Monitor EUT performance for susceptibility
effects.
(c) Ensure that the E-field sensor is indicating the field from the fundamental
frequency and not from the harmonics.
(2) Receive antenna procedure.
(a) Remove the receive antenna and reposition the EUT in conformance with
5.20.3.3a.
(b) Set the signal source to 1 kHz pulse modulation, 50% duty cycle. Using an
appropriate amplifier and transmit antenna, establish an electric field at the
test start frequency. Gradually increase the input power level until it
corresponds to the applicable level recorded during the calibration routine.
(c) Scan the required frequency range in accordance with the rates and durations
specified in Table III while assuring the correct transmitter input power is
adjusted in accordance with the calibration data collected. Constantly
monitor the EUT for susceptibility conditions.
(3) If susceptibility is noted, determine the threshold level in accordance with
4.3.10.4.3 and verify that it is above the limit.
(4) Perform testing over the required frequency range with the transmit antenna
vertically polarized. Repeat the testing above 30 MHz with the transmit antenna
horizontally polarized.
(5) Repeat 5.20.3.4d for each transmit antenna position required by 5.20.3.3e.
5.20.3.5 Data presentation.
Data presentation shall be as follows:
a. Provide graphical or tabular data showing frequency ranges and field strength levels
tested.
b. Provide graphical or tabular data listing (antenna procedure only) all calibration data
collected to include input power requirements used versus frequency, and results of
system check in 5.20.3.4c(2)(c) and 5.20.3.4c(2)(d).
c. Provide the correction factors necessary to adjust sensor output readings for equivalent
peak detection of modulated waveforms.
d. Provide graphs or tables listing any susceptibility thresholds that were determined along
with their associated frequencies.

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 MIL-STD-461F

e. Provide diagrams or photographs showing actual equipment setup and the associated
dimensions.
5.20.4 RS103 alternative test procedures – reverberation chamber (mode-tuned).
These procedures may be substituted for the 5.20.3 procedures over the frequency range of 200
MHz to 40 GHz. The lower frequency limit is dependent on chamber size. To determine the
lower frequency limit for a given chamber, use the following formula to determine the number of
possible modes (N) which can exist at a given frequency. If, for a given frequency, N is less
than 100 then the chamber should not be used at or below that frequency.
8π f 3
N = abd 3
3 c
where: a, b, and d are the chamber internal dimensions in meters
f is the operation frequency in Hz
c is the speed of propagation (3 x 108 m/s)
5.20.4.1 Purpose.
This test procedure is an alternative technique used to verify the ability of the EUT and
associated cabling to withstand electric fields.
5.20.4.2 Test equipment.
The test equipment shall be as follows:
a. Signal generators
b. Power amplifiers
c. Receive antennas
(1) 200 MHz to 1 GHz, log periodic or double ridge horns.
(2) 1 GHz to 18 GHz, double ridge horns.
(3) 18 GHz to 40 GHz, other antennas as approved by the procuring activity.
d. Transmit antennas
e. Electric field sensors (physically small - electrically short), each axis independently
displayed
f. Measurement receiver
g. Power meter
h. Directional coupler
i. Attenuator, 50 ohm
j. Data recording device
k. LISNs
5.20.4.3 Setup.
The test setup shall be as follows:

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 MIL-STD-461F

a. Install the EUT in a reverberation chamber using the basic test setup for the EUT as
shown and described in Figures 2 through 5 and 4.3.8. The EUT shall be at least 1.0
meter from the chamber walls, the tuner, and antennas.
b. For electric field calibration, electric field sensors (5.20.4.2e) are required from 200
MHz to 1 GHz. Either field sensors or receive antennas may be used above 1 GHz (see
5.20.4.2c and 5.20.4.2e).
c. Configure the test equipment as shown in Figures RS103-5 and RS103-6. The same
configuration is used for both calibration and EUT testing. The transmit and receive
antennas shall be present in the chamber for all calibration and EUT testing, including
for the electric-field probe technique. Unused receive antennas shall be terminated in
50 ohms.
5.20.4.4 Procedure.
The test procedures shall be as follows:
a. Calibration. Use the following procedure to determine the electric field strength that
will be created inside the chamber when a fixed amount of RF energy is injected into
the chamber.
(1) Receive antenna procedure.
(a) Adjust the RF source to inject an appropriate forward power (unmodulated)
into the chamber at the start frequency of the test.
(b) Measure the level at the receive antenna using the measurement receiver.
(c) Rotate the tuner 360 degrees using the minimum number of steps required
from Table VIII. Allow the paddle wheel to dwell at each position for a
period corresponding to a minimum of 1.5 times the response time of the
measurement receiver.
(d) Record the maximum amplitude of the signal received and use the following
formula to derive a calibration factor for the field strength created inside the
chamber. (Pr-max and Pforward in watts; λ in meters).

8π Pr − max
Calibration factor = 5( ) V/m (for one watt)
λ Pforward

(e) Repeat the procedure in frequency steps no greater than 2% of the preceding
frequency until 1.1 times the start frequency is reached. Continue the
procedure in frequency steps no greater than 10% of the preceding frequency,
thereafter.
(2) Electric field probe procedure.
(a) Adjust the RF source to inject an appropriate forward power (Pforward)
(unmodulated) into the chamber at the start frequency of the test.
(b) Rotate the tuner 360 degrees using the minimum number of steps required
from Table VIII. Allow the tuner to dwell at each position for a period
corresponding to a minimum of 1.5 times the probe response time.

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 MIL-STD-461F

(c) Record the maximum amplitude from the receive antenna (Pr-max) and from
each element of the probe and use the following formula to derive a
calibration factor for the field strength created inside the chamber. (Probe
reading in V/m and Pforward in watts).
E x − max + E y − max + E z − max
( )2
Calibration factor = 3 V/m (for one watt)
Pforward

(d) Repeat the procedure in frequency steps no greater than 2% of the preceding
frequency until 1.1 times the start frequency is reached. Continue the
procedure in frequency steps no greater than 10% of the preceding frequency,
thereafter.
b. EUT testing. The same antennas used for calibration shall be used for EUT
testing.
(1) Turn on the measurement equipment and allow a sufficient time for
stabilization.
(2) Set the RF source to the start frequency of the test with 1 kHz pulse
modulation, 50 % duty cycle.
(3) Calculate the amount of RF power needed to create the desired field strength
by determining the difference (in dB - decibel differences are the same for
both field strength and power, there is a square law relationship between field
strength and power in real numbers) between the desired field strength and
the field strength obtained during the calibration. Adjust the chamber peak
forward power to this value. Interpolation between calibration points is
required.
(4) Adjust the measurement receiver to display the received signal at the receive
antenna to verify that an electric field is present.
(5) Rotate the tuner 360 degrees using the minimum of steps shown in Table
VIII. Allow the tuner to dwell at each position for the duration specified in
Table III. As the tuner rotates, maintain the forward power required to
produce field levels at the applicable limit as determined from the calibration.
(6) Scan the required frequency range in accordance with the maximum
frequency step sizes and durations specified in Table III. Monitor EUT
performance for susceptibility effects.
(7) If susceptibility is noted, determine the threshold level in accordance with
4.3.10.4.3 and verify that it is above the limit.
5.20.4.5 Data presentation.
Data presentation shall be as follows:
a. Provide graphical or tabular data showing frequency ranges and field strength levels
tested.

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 MIL-STD-461F

b. Provide graphical or tabular data listing of all calibration data collected to include input
power requirements used versus frequency and results of calibration in 5.20.4.4a(1)(d)
and 5.20.4.4a(2)(c).
c. Provide the correction factors necessary to adjust sensor output readings for equivalent
peak detection of modulated waveforms.
d. Provide graphs or tables listing any susceptibility thresholds that were determined along
with their associated frequencies.
e. Provide diagrams or photographs showing the actual equipment setup and the
associated dimensions.
f. Provide the data certifying the baseline performance of the shielded room as a properly
functioning reverberation chamber over a defined frequency range.

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 TABLE VII. RS103 limits.

LIMIT LEVEL (VOLTS/METER)

PLATFORM ALL SHIPS
AIRCRAFT
(ABOVE DECKS) SHIPS SHIPS (NON-
(EXTERNAL OR AIRCRAFT
AND (METALLIC) METALLIC) SUBMARINES GROUND SPACE
SAFETY INTERNAL
SUBMARINES (BELOW DECKS) (BELOW DECKS) (INTERNAL)
FREQ. CRITICAL)
(EXTERNAL)*
RANGE **
2 MHz A 200 200 200 10 50 5 50 20
N 200 200 200 10 50 5 10 20
30 MHz AF 200 20 - - - - 10 20
30 MHz A 200 200 200 10 10 10 50 20

135
N 200 200 200 10 10 10 10 20
1 GHz AF 200 20 - - - - 10 20
MIL-STD-461F

1 GHz A 200 200 200 10 10 10 50 20

N 200 200 200 10 10 10 50 20
TABLE VII. RS103 limits.

18 GHz AF 200 60 - - - - 50 20
18 GHz A 200 200 200 10 10 10 50 20
N 200 60 200 10 10 10 50 20

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40 GHz AF 200 60 - - - - 50 20

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KEY: A = Army * For equipment located external to the pressure hull of a submarine but within the superstructure, use
N = Navy SHIPS (METALLIC)(BELOW DECKS)
AF = Air Force
** Equipment located in the hanger deck of Aircraft Carriers

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RS103
 MIL-STD-461F

TABLE VIII. Required number of tuner positions for a reverberation chamber.

Frequency Range
(MHz) Tuner Positions
200 - 300 50
300 - 400 20
400 - 600 16
Above 600 12

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 MIL-STD-461F

TEST SETUP BOUNDARY

Electric
Field
Sensor LISN

EUT

3m
1.5 m

Antenna

Shielded Enclosure

RF Stimulation
Amplifiers and Monitoring
Equipment

Signal Electric Field

Source Sensor Display

FIGURE RS103-1. Test equipment configuration.

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 MIL-STD-461F

TEST SETUP BOUNDARY

LISN Electric
Field
Sensor

EUT EUT EUT

N Antenna
Positions

Shielded Enclosure

RF Stimulation
Amplifiers and Monitoring
Equipment

Signal Electric Field

Source Sensor Display

FIGURE RS103-2. Multiple test antenna locations for frequency > 200 MHz.

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 MIL-STD-461F

TEST SETUP BOUNDARY

D > 3 Meters

LISN

EUT EUT
N Electric Field Sensor
Positions

D D
N N

N Antenna Positions
Shielded Enclosure

RF Stimulation
Amplifiers and Monitoring
Equipment

Signal Electric Field

Source Sensor Display

FIGURE RS103-3. Multiple test antenna locations for N positions, D > 3 meters.

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 MIL-STD-461F

TEST SETUP BOUNDARY

Signal
Generator
Path for Path for
Measurement System Check

Receive
Antenna

Transmit
Antenna

Shielded Enclosure

Signal
Source Attenuator

RF Measurement
Amplifiers Receiver

Directional Data
Coupler Recorder

Power
Meter

Data
Recorder

FIGURE RS103-4. Receive antenna procedure (1 to 40 GHz).

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 MIL-STD-461F

Chamber

1.0 Meter Minimum

Test Setup Boundary

Receive Antenna
(present at all times, if used)
Transmit or
Antenna
E-field Probe
Tuner(s)

Stepping
Motor

Forward Attenuator
Directional (Incident) Power
or
Coupler Meter Probe Display

Power Motor Measurement

Amplifier Controller Receiver

Signal
Source

FIGURE RS103-5. Reverberation chamber setup.

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 MIL-STD-461F

Alternative Position
for Tuner
Tuner

Drive
Reverberation Motor
Chamber

Incoming
Mains Power Ground Plane
Filter Electrically Bonded
to Floor

LISNs
Tuner
EUT

1 Meter

Volume of
Uniform Field

Bulkhead/Filter
Penetrations Field Generation Antenna
Pointed into Corner of
Chamber with Tuner

Shielded
Field Generation Side-Chamber
EUT Monitoring
Equipment and Equipment and
Electrical Loads Motor Controller

FIGURE RS103-6. Reverberation chamber overview.

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 MIL-STD-461F

5.21 RS105, radiated susceptibility, transient electromagnetic field.

5.21.1 RS105 applicability.

This requirement is applicable to equipment and subsystem enclosures when the equipment or
subsystem is to be located external to a hardened (shielded) platform or facility. The
requirement is applicable for equipment intended solely for use on non-metallic platforms when
specified by the procuring activity. The requirement is applicable to Army aircraft for safety
critical equipment and subsystems located in an external installation.
5.21.2 RS105 limit.
The EUT shall not exhibit any malfunction, degradation of performance, or deviation from
specified indications, beyond the tolerances indicated in the individual equipment or subsystem
specification, when subjected to a test signal having the waveform and amplitude shown on
Figure RS105-1. At least five pulses shall be applied at the rate of not more than one pulse per
minute.
5.21.3 RS105 test procedures.

5.21.3.1 Purpose.
This test procedure is used to verify the ability of the EUT enclosure to withstand a transient
electromagnetic field.
5.21.3.2 Test equipment.
The test equipment shall be as follows:
a. Transverse electromagnetic (TEM) cell, parallel plate transmission line or equivalent
b. Transient pulse generator, monopulse output, plus and minus polarity
c. Storage oscilloscope, 500 MHz, single-shot bandwidth (minimum), variable sampling
rate up to 1gigasample per second (GSa/s)
d. Terminal protection devices
e. High-voltage probe, 1 GHz bandwidth (minimum)
f. B-dot sensor probe
g. D-dot sensor probe
h. LISNs
i. Integrator, time constant ten times the overall pulse width
5.20.3.3 Setup.
Set up the EUT as described below. CAUTION: Exercise extreme care if an open radiator is
used for this test.
a. Calibration. Configure the test equipment in accordance with Figure RS105-2.
(1) Before installing the EUT in the test volume, place the B-dot or D-dot sensor
probe in the center position of the five point grid in the vertical plane where the
front face of the EUT will be located (see Figure RS105-2).

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 MIL-STD-461F

(2) Place the high-voltage probe across the input to the radiation system at the output
of the transient pulse generator. Connect the probe to a storage oscilloscope.
b. EUT Testing. Configure the test equipment as shown in Figure RS105-3 for testing of
the EUT.
(1) Place the EUT centerline on the centerline of the working volume of the radiation
system in such a manner that it does not exceed the usable volume of the radiation
system (h/3, B/2, A/2)/(x,y,z) as shown in Figure RS105-3 (h is the maximum
vertical separation of the plates). If the EUT is mounted on a ground plane in the
actual installation, the EUT shall be placed on the radiating system ground plane.
The EUT shall be bonded to the ground plane in a manner that duplicates the
actual installation. Otherwise, the EUT shall be supported by dielectric material
that produces a minimum distortion of the EM fields.
(2) The EUT orientation shall be such that the maximum coupling of electric and or
magnetic fields is simulated. This may require more than one test orientation.
(3) Cables for EUT operation and monitoring shall be oriented to minimize induced
currents and voltages on the cables. Cabling shall be oriented normal to the
electric field vector and in a manner that minimizes the loop area normal to the
magnetic field vector. Cables extending out of the parallel plate working volume
should remain normal to the electric field vector for a minimum distance equal to
2 times h.
(4) Bond the bottom plate of the radiation system to an earth reference.
(5) Keep the top plate of the radiation system at least 2 times h from the closest
metallic ground, including ceiling, building structural beams, metallic air ducts,
shielded room walls, and so forth.
(6) Place the EUT actual or simulated loads and signals for electrical interfaces in a
shielded enclosure when an open radiator is used.
(7) Place TPDs in the EUT power lines near the power source to protect the power
source.
(8) Connect the transient pulse generator to the radiation system.
5.21.3.4 Procedures.
The test procedures shall be as follows:
a. Turn on the measurement equipment and allow a sufficient time for stabilization.
b. Calibration. Perform the following procedures using the calibration setup:
(1) Generate a pulse and adjust the pulse generator to produce a pulsed field, as
measured with the B-dot or D-dot probes, which meets the peak amplitude, rise
time, and pulse width requirements. CAUTION: High voltages are used which are
potentially lethal. Record the drive pulse waveform as displayed on the
oscilloscope.
(2) Tolerances and characteristics of the RS105 limit shall be as follows:

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 MIL-STD-461F

(a) rise time (between 10% and 90% points) between 1.8 ns and 2.8 ns (electric
field continuously increasing).
(b) full width half maximum (FWHM) pulse width equal to 23 ns ± 5 ns.
(c) peak value of the electric or magnetic field for each grid position:
0 dB ≤ magnitude ≤ 6 dB above limit.
(3) Repeat steps (1) and (2) above for the other four test points on Figure RS105-2.
(4) Determine the pulse generator settings and associated pulse drive amplitude
which simultaneously satisfies the field requirements for all five grid positions.
c. EUT Testing. Perform the following procedures using the test setup:
(1) Turn on the EUT and allow sufficient time for stabilization.
(2) Test the EUT in its orthogonal orientations whenever possible.
(3) Apply the pulse starting at 10% of the pulse peak amplitude determined in
5.21.3.4b(4) with the specified waveshape where practical. Increase the pulse
amplitude in step sizes of 2 or 3 until the required level is reached.
(4) Ensure that the drive pulse waveform characteristics at the required test level are
consistent with those noted in 5.21.3.4b(2).
(5) Apply the required number of pulses at a rate of not more than 1 pulse per minute.
(6) Monitor the EUT during and after each pulse for signs of susceptibility or
degradation of performance.
(7) If an EUT malfunction occurs at a level less than the specified peak level,
terminate the test and record the level.
(8) If susceptibility is noted, determine the threshold level in accordance with
4.3.10.4.3 and verify that it is above the limit.
5.21.3.5 Data presentation.
Data presentation shall be as follows:
a. Provide photographs of EUT orientation including cables.
b. Provide a detailed written description of the EUT configuration.
c. Provide oscilloscope recordings that show peak value, rise time, and pulse width of one
applied pulse for each EUT orientation.
d. Provide the pulse number, with the first pulse being Number 1, for each recorded
waveshape.
e. Record the time-to-recovery for each EUT failure, if applicable.

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 MIL-STD-461F

60000
E1(t) = 0 when t < 0
− a1t − b1t
= E01 x k1 ( e −e ) when t > 0
50000

E01 = 5 x 104 V/m

Field strength (V/m)

40000 a1 = 4 x 107 s-1

b1 = 6 x 108 s-1

30000 k1 = 1.3

20000

10000

0
0 10 20 30 40 50 60 70 80 90 100
Time (Nanoseconds)

FIGURE RS105-1. RS105 limit for all applications.

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 MIL-STD-461F

Less than 0.5 dB

loss at 200 MHz

FIGURE RS105-2. Typical calibration setup using parallel plate radiation system.

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 MIL-STD-461F

TOP VIEW

Oscilloscope

Shielded
Enclosure

A
HV
Transient
Probe
Pulse A/2
Generator

B B/2 EUT

Usable Test Volume Cable in Conduit

(Centered on Bottom Plate) (Beneath Bottom Plate)

Power Line

Actual and
LISN Simulated Loads
and Signals

TPDs

Shielded
Enclosure
Power Input

FIGURE RS105-3. Typical test setup using parallel plate radiation system.

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 MIL-STD-461F

6. NOTES
(This section contains information of a general or explanatory nature that may be helpful, but is
not mandatory.)
6.1 Intended use.
This standard is intended for use in the acquisition cycle of equipment and subsystems to specify
the electromagnetic emission and susceptibility requirements for the control of EMI.
6.2 Acquisition requirements.
Acquisition documents should specify the following:
a. Title, number, and date of the standard.
6.3 Associated Data Item Descriptions (DIDs).
This standard has been assigned an Acquisition Management Systems Control (ASMC) number
authorizing it as the source document for the following DIDs. When it is necessary to obtain the
data, the applicable DIDs must be listed on the Contract Data Requirements List (DD Form
1423).

DID Number DID Title

DI-EMCS-80199C Electromagnetic Interference
Control Procedures (EMICP)
DI-EMCS-80201C Electromagnetic Interference
Test Procedures (EMITP)
DI-EMCS-80200C Electromagnetic Interference
Test Report (EMITR)

The above DIDs were current as of the date of this standard. The ASSIST database should be
researched at http://assist.daps.dla.mil/quicksearch/ to ensure that only current and approved
DIDs are cited on the DD Form 1423.
6.4 Tailoring guidance.
Application specific criteria may be derived from operational and engineering analyses on the
equipment or subsystem being procured for use in specific environments. When analyses reveal
that a requirement in this standard is not appropriate or adequate for that procurement, the
requirement should be tailored and incorporated into the appropriate documentation, prior to
contract award or through contractual modification early in the developmental phase. The
appendix of this standard provides guidance for tailoring.
6.5 Subject term (key word) listing.
EMC
EMI
Electromagnetic compatibility
Electromagnetic emission
Electromagnetic interference

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 MIL-STD-461F

Electromagnetic susceptibility
Test Limits, EMI
6.6 International standardization agreement implementation.
This standard implements STANAG 3516 (Electromagnetic Interference, Test Methods for
Aircraft Electrical and Electronic Equipment) and STANAG 4370 (Environmental Testing).
When changes to, revision, or cancellation of this standard are proposed, the preparing activity
must coordinate the action with the U.S. National Point of Contact for the international
standardization agreement, as identified in the ASSIST database at http://assist.daps.dla.mil.
6.7 Changes from previous issue.
Marginal notations are not used in the revision to identify changes with respect to the previous
issue due to the extensiveness of the changes.
6.8 Technical points of contact.
Requests for additional information or assistance on this standard can be obtained from the
following:
a. Commander, U.S. Army, AMCOM
AMSRD-AMR-AE-S
Building 4488
Redstone Arsenal, AL 35898
Mr. Dave Lewey
DSN 897-8464; Commercial (256) 313-8464
E-mail: Dave.Lewey@us.army.mil
b. Naval Air Systems Command
Code: 4.1.13
48110 Shaw Rd
Building 2187
Patuxent River, MD 20670
Mr. Robert Smith
DSN 342-9223; Commercial (301) 342-9223
E-mail: Robert.B.Smith5@navy.mil
c. ASC/ENAD, Building 560
2530 Loop Road West
Wright Patterson AFB, OH 45433-7101
Mr. Manny Rodriguez
DSN 785-8928; Commercial (937) 255-8928
E-mail: Manuel.Rodriguez@wpafb.af.mil
Any information relating to Government contracts must be obtained through contracting officers.

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APPLICATION GUIDE

A.1 GENERAL

A.1.1 Scope.
This appendix provides background information for each emission and susceptibility and
associated test requirement in the main body of the standard. This information includes rationale
for requirements, guidance in applying the requirements, and lessons learned from platform and
laboratory experience. This information should help users understand the intent behind the
requirements, should aid the procuring activity in tailoring emission and susceptibility
requirements as necessary for particular applications, and should help users develop detailed test
procedures in the EMITP based on the general test procedures in this document. This appendix
is provided for guidance purposes and, as such, should not be interpreted as providing
contractual requirements.
A.1.2 Structure.
This appendix follows the same general format as the main body of the standard. Section 4
general requirements from the main body are repeated in this appendix and are in italics. Main
body paragraph numbers corresponding to each requirement are included in parentheses. A
"Discussion" paragraph is provided for each requirement. Though section 5 detailed
requirements from the main body are not repeated, discussion paragraphs on “Applicability and
limits” and “Test procedure” are included.

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A.2 APPLICABLE DOCUMENTS

A.2.1 General.
The documents listed in this section are specified within this appendix.
A.2.2 Government documents.

A.2.2.1 Specifications, standards, and handbooks.

The following specifications, standards, and handbooks specified herein are referenced solely to
provide supplemental technical data. These documents are for informational purposes only.

DEPARTMENT OF DEFENSE STANDARDS

MIL-STD-188-125-1 - HEMP Protection for Ground-Based C4I

Facilities Performing Critical, Time-Urgent
Missions Part 1 Fixed Facilities
MIL-STD-464 – Electromagnetic Environmental Effects
Requirements for Systems
MIL-STD-704 – Aircraft Electric Power Characteristics
MIL-STD-1275 – Characteristics of 28 Volt DC Electrical
Systems in Military Vehicles
MIL-STD-1399-300A – Interface Standard for Shipboard Systems,
(NAVY) Section 300A, Electric Power, Alternating
Current
MIL-STD-1539 – Electric Power, Direct Current, Space Vehicle
(USAF) Design Requirements

DEPARTMENT OF DEFENSE HANDBOOKS

MIL-HDBK-235/1 – Electromagnetic (Radiated) Environment
Considerations for Design and Procurement of
Electrical and Electronic Equipment
MIL-HDBK-237 – Electromagnetic Environmental Effects and
Spectrum Supportability Guidance for the
Acquisition Process
MIL-HDBK-423 – HEMP Protection for Fixed and Transportable
Ground-Based Facilities
(Copies of these documents are available online at http://assist.daps.dla.mil/quicksearch/ or
from the Standardization Document Order Desk, 700 Robbins Avenue, Building 4D,
Philadelphia, PA 19111-5094. [Telephone 215-697-6396].)

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A.2.2.2 Other Government documents, drawings, and publications.

The following other Government documents, drawings, and publications specified herein are
referenced solely to provide supplemental technical data. These documents are for informational
purposes only.

AIR FORCE
AFSC DH 1-4 – Air Force Systems Command Design
Handbook, EMC
AFI 11-202V3 – General Flight Rules

FEDERAL COMMUNICATIONS COMMISSION

CFR Title 47 – Parts 2, 15, and 18

DEPARTMENT OF DEFENSE (DoD)

DoDI 6055.11 – Protection of DoD Personnel from Exposure to
Radio Frequency Radiation and Military
Exempt Lasers
SD-2 – Buying Commercial and Nondevelopmental
Items

NATIONAL BUREAU OF STANDARDS (NBS)

Technical Note 1092 – Design, Evaluation, and Use of a Reverberation
Chamber for Performing Electromagnetic
Susceptibility/Vulnerability Measurements

NATIONAL INSTITUTE OF SCIENCE AND TECNOLOGY (NIST)

Technical Note 1508 – Evaluation of the NASA Langley Research
Center Mode-Stirred Chamber Facility

NATIONAL TELECOMMUNICATION AND INFORMATION AGENCY (NTIA)

NTIA – Manual of Regulations & Procedures for
Federal Radio Frequency Management

NAVY
NAVSEA OD 30393 – Design Principles and Practices for Controlling
Hazards of Electromagnetic Radiation to
Ordnance

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ARMY
AMC Pamphlet 706-235 – Hardening Weapon Systems Against RF
Energy
AMC Pamphlet 706-410 – Engineering Design Handbook, EMC
ADS-37A-PRF – Electromagnetic Environmental Effects (E3)
Design And Verification Requirements
AR 40-61 – Medical Logistics Policies
AR 70-62 – Airworthiness Certification of US Army
Aircraft Systems
(Application for copies of National Bureau of Standards and National Institute for Science
and Technology documents should be addressed to NIST Public Inquiries, Administration
Building, A903, National Institute for Science and Technology (NIST), Gaithersburg MD
20899-0001 [Telephone: 301-975-3058], http://www.nist.gov/. Copies of other publications
required by contractors in connection with specific acquisition functions should be obtained from
the contracting activity or as directed by the contracting officer.)
A.2.3 Non-Government publications.
The following non-government documents specified herein are referenced solely to provide
supplemental technical data. These documents are for informational purposes only.
AMERICAN NATIONAL STANDARDS INSTITUTE (ANSI)
ANSI/IEEE C63.2 – Standard for Instrumentation, Electromagnetic
Noise and Field Strength, 10 kHz to 40 GHz,
Specifications
ANSI/IEEE C63.4 – Standard for Electromagnetic Compatibility,
Radio-Noise Emissions from Low Voltage
Electrical and Electronic Equipment in the
Range of 9 kHz to 1 GHz, Methods of
Measurement
ANSI/IEEE C63.12 – Standard for Electromagnetic Compatibility
Limits, Recommended Practice
ANSI/IEEE C63.14 – Standard Dictionary for Technologies of
Electromagnetic Compatibility (EMC),
Electromagnetic Pulse (EMP), and Electrostatic
Discharge (ESD)
ANSI/NCSL Z540-1 – General Requirements for Calibration
Laboratories and Measuring and Test
Equipment
(Application for copies should be addressed to the American National Standards Institute,
11 West 42nd Street, New York, New York 10036 [Telephone: 212-642-4900 or Fax:
212-398-0023], http://www.ansi.org/; or the Institute of Electrical and Electronics Engineers,

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Incorporated (IEEE), 445 Hoes Lane, Piscataway, NJ 08855-1331 [Telephone: 800-701-4333 or

Fax: 908-981-9667]. http://www.ieee.org/portal/site.)

AMERICAN SOCIETY FOR TESTING AND MATERIALS (ASTM)

ASTM SI 10 – American National Standard for Use of the
International System of Units (SI): The Modern
Metric System
(Application for copies should be addressed to the American Society for Testing and
Materials, 1916 Race Street, Philadelphia PA 19103-1187 [Telephone: 215-299-5585 or FAX:
215-977-9679], http://www.astm.org/.)

INTERNATIONAL ELECTROTECHNIC COMMISSION (IEC)

IEC 61000-4-21 – Electromagnetic Compatibility (EMC) Part 4-
21: Testing and Measurement Techniques –
Reverberation Chamber Test Methods
(Application for copies should be addressed to the American National Standards Institute,
11 West 42nd Street, New York, New York 10036 [Telephone: 212-642-4900 or Fax: 212-398-
0023], http://www.ansi.org/.)

INTERNATIONAL STANDARDIZATION ORGANIZATION (ISO)

ISO 10012 – Measurement Management Systems –
Requirements for Measurement Processes and
Measuring Equipment
(Application for copies of ISO documents should be addressed to ISO, International
Organization for Standardization, 3 rue de Varembe, 1211 Geneve 20, Geneve, Switzerland
[Telephone: 41 22 734 0150], http://www.iso.org/iso/home.htm.)

NATIONAL FIRE PROTECTION ASSOCIATION (NFPA)

National Electrical Code
(Application for copies should be addressed to the National Fire Protection Association, One
Batterymarch Park, Quincy MA 02269-9990 [Telephone: 617-770-3000 or FAX: 617-770-
0700], http://www.nfpa.org/.)

RADIO TECHNICAL COMMISSION FOR AERONAUTICS

DO-160 – Environmental Conditions and Test Procedures
for Airborne Equipment
(Applications for copies should be addressed to Radio Technical Commission for
Aeronautics Secretariat, One McPherson Square, Suite 500, 1425 K Street, NW, Washington DC
20005, http://www.rtca.org/.)

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SOCIETY OF AUTOMOTIVE ENGINEERS (SAE)

ARP 958 – Electromagnetic Interference Measurement
Antennas; Standard Calibration Method
ARP 1972 – Recommended Measurement Practices and
Procedures for EMC Testing
(Application for copies should be addressed to the Society of Automotive Engineers,
Incorporated, 400 Commonwealth Drive, Warrendale, PA 15096 [Telephone: 412-776-4841 or
FAX: 412-776-5760], http://www.sae.org/.)
(Non-government standards are generally available for reference from libraries. They are
also distributed among non-government standards bodies and using Federal agencies.)

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A.3 DEFINITIONS

A.3.1 General.
The terms used in this appendix are defined in ANSI C63.14. In addition, the following
definitions are applicable for the purpose of this appendix.
A.3.2 Acronyms used in this appendix.
ASW - Anti-submarine Warfare
BIT - Built-in-Test
CI - Commercial Item
CW - Continuous Wave
DoD - Department of Defense
E3 - Electromagnetic Environmental Effects
ECM - Electronic Countermeasures
EMC - Electromagnetic Compatibility
EME - Electromagnetic Environment
EMI - Electromagnetic Interference
EMICP - Electromagnetic Interference Control Procedures
EMITP - Electromagnetic Interference Test Procedures
EMITR - Electromagnetic Interference Test Report
EMP - Electromagnetic Pulse
ERP - Effective Radiated Power
EUT - Equipment Under Test
FCC - Federal Communication Commission
GPI - Ground Plane Interference
GFE - Government Furnished Equipment
HPM - High Power Microwave
LISN - Line Impedance Stabilization Network
NDI - Non-Developmental Item
NOE - Nap-of-the-earth
RF - Radio Frequency
RMS - Root Mean Square
TEM - Transverse Electromagnetic
TPD - Terminal Protection Device

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UPS - Uninterruptible Power Supplies

VFR - Visual Flight Rules
VSWR - Voltage Standing Wave Ratio

A.3.3 Below deck.

An area on ships which is surrounded by a metallic structure, or an area which provides
significant attenuation to electromagnetic radiation, such as the metal hull or superstructure of a
surface ship, the pressure hull of a submarine and the screened rooms in non-metallic ships.
A.3.4 External installation.
An equipment location on a platform which is exposed to the external electromagnetic
environment, such as an aircraft cockpit which does not use electrically conductive treatments on
the canopy or windscreen.
A.3.5 Internal installation.
An equipment location on a platform which is totally inside an electrically conductive structure,
such as a typical avionics bay in an aluminum skin aircraft.
A.3.6 Metric units.
Metric units are a system of basic measures which are defined by the International System of
Units based on "Le System International d'Unites (SI)," of the International Bureau of Weights
and Measures. These units are described in ASTM SI 10.
A.3.7 Non-developmental item.
Non-developmental item is a broad, generic term that covers material available from a wide
variety of sources with little or no development effort required by the Government.
A.3.8 Safety critical.
A category of subsystems and equipment whose degraded performance could result in loss of life
or loss of vehicle or platform.
A.3.9 Test setup boundary.
The test setup boundary includes all enclosures of the Equipment Under Test (EUT) and the 2
meters of exposed interconnecting leads (except for leads which are shorter in the actual
installation) and power leads required by 4.3.8.6.

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A.4 GENERAL REQUIREMENTS

A.4.1 (4.1) General.

Electronic, electrical, and electromechanical equipment and subsystems shall comply with the
applicable general interface requirements in 4.2. General requirements for verification shall be
in accordance with 4.3. These general requirements are in addition to the applicable detailed
emission and susceptibility requirements and associated test procedures defined in 5.
Discussion: The requirements in this paragraph are universally applicable to all subsystems and
equipment. Separate emission and susceptibility requirements that are structured to address
specific concerns with various classes of subsystems and equipment are contained in other
portions of this standard.
This document is concerned only with specifying technical requirements for controlling
electromagnetic interference (EMI) emissions and susceptibility at the subsystem-level and
equipment-level. The requirements in this document are not intended to be directly applied to
subassemblies of equipment such as modules or circuit cards. The basic concepts can be
implemented at the subassembly level; however, significant tailoring needs to be accomplished
for the particular application. The requirements included herein are intended to be used as a
baseline. Placement of the limits is based on demonstrated performance typically required for
use on existing platforms in order to achieve electromagnetic compatibility. System-level
requirements dealing with integration of subsystems and equipment are contained in documents
such as MIL-STD-464 and MIL-STD-188-125-1. MIL-STD-464 requirements include intra-
system compatibility within the system, inter-system compatibility with external radio frequency
environments, lightning protection, and hazards of electromagnetic radiation to ordnance, fuel
and personnel. The procuring activity and system contractors should review the requirements
contained herein for possible tailoring based on system design and expected operational
environments. NTIA “Manual of Regulations and Procedures for Federal Radio Frequency
Management” provides requirements for complying with laws governing use of the radio
frequency spectrum by federal agencies.
Guidance and techniques which are helpful in meeting the requirements of this standard are
contained in MIL-HDBK-423, AFSC DH 1-4, and AMC Pamphlet 706-410. MIL-HDBK-237
provides guidance for management of Electromagnetic Environmental Effects (E3) efforts.
ADS-37A-PRF provides additional guidance for Army equipment located or operated on fixed-
wing aircraft and helicopters. MIL-HDBK-235/1 provides information on land, air, and sea based
RF emitters, both hostile and friendly, which contribute to the overall EME.
The qualification status of equipment and subsystems becomes uncertain when hardware or
software changes are incorporated due to equipment updates or test failures, including failures
from testing to requirements other than EMI. To maintain certification to MIL-STD-461 after
changes are implemented, either an analysis showing no substantive impact needs to be issued or
continued compliance needs to be demonstrated by limited testing deemed to be appropriate to
evaluate the changes. The approach used to maintain continued certification and the results of
analysis and testing are normally subject to procuring activity approval.

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A.4.2 (4.2) Interface Requirements.

A.4.2.1 (4.2.1) Joint procurement.

Equipment or subsystems procured by one DoD activity for multi-agency use shall comply with
the requirements of the user agencies.
Discussion: When the government procures equipment that will be used by more than one
service or agency, a particular activity is assigned responsibility for overall procurement. The
responsible activity must address the concerns of all the users. Conflicts may exist among the
parties concerned. Also, imposition of more severe design requirements by one party may
adversely affect other performance characteristics required by the second party. For example,
severe radiated susceptibility levels on an electro-optical sensor may require aperture protection
measures which compromise sensitivity. It is important that these issues be resolved to the
satisfaction of all parties and that all genuine requirements be included.
A.4.2.2 (4.2.2) Filtering (Navy only).
The use of line-to-ground filters for EMI control shall be minimized. Such filters establish low
impedance paths for structure (common-mode) currents through the ground plane and can be a
major cause of interference in systems, platforms, or installations because the currents can
couple into other equipment using the same ground plane. If such a filter must be employed, the
line-to-ground capacitance for each line shall not exceed 0.1 microfarads (µF) for 60 Hertz (Hz)
equipment or 0.02 µF for 400 Hz equipment. For submarine DC-powered equipment and
aircraft DC-powered equipment, the filter capacitance from each line-to-ground at the user
interface shall not exceed 0.075 µF/kW of connected load. For DC loads less than 0.5 kW, the
filter capacitance shall not exceed 0.03 µF. The filtering employed shall be fully described in
the equipment or subsystem technical manual and the Electromagnetic Interference Control
Procedures (EMICP) (see 6.3).
Discussion: The power systems for Navy ships and submarines are ungrounded. The
capacitance-to-ground of power line filters provides a path for conducting current into the hull
structure. The Navy uses very sensitive low frequency radio and sonar receivers. At low
frequencies, currents flowing through the installation structure and across surfaces of electronic
enclosures will penetrate to the inside of the enclosure. The magnetic fields created by these
currents can couple into critical circuits and degrade performance. At higher frequencies
(greater than 100 kHz), the combination of power line filter capacitance-to-ground limitation,
skin effect of equipment enclosures, and reduced harmonic currents tend to minimize the
problems associated with structure currents.
The total line-to-ground capacitance is limited to 0.1 μf for 60 Hz equipment and 0.02 μf for 400
Hz equipment. This will, in turn, limit the power line current to 5 mA which is consistent with
leakage current (safety) requirements. The filtering employed should be fully described in the
Electromagnetic Interference Control Procedures.

A.4.2.3 (4.2.3) Self-compatibility.

The operational performance of an equipment or subsystem shall not be degraded, nor shall it
malfunction, when all of the units or devices in the equipment or subsystem are operating
together at their designed levels of efficiency or their design capability.

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Discussion: The EMI controls imposed by this standard apply to subsystem-level hardware with
the purpose of insuring compatibility when various subsystems are integrated into a system
platform. In a parallel sense, a subsystem can be considered to be an integration of various
assemblies, circuit cards, and electronics boxes. While specific requirements could be imposed
to control the interference characteristics of these individual items, this standard is concerned
only with the overall performance characteristics of the subsystem after integration. Therefore,
the subsystem itself must exhibit compatibility among its various component parts and
assemblies.
A.4.2.4 (4.2.4) Non-Developmental Items (NDI).
In accordance with the guidance provided by DoD SD-2, the requirements of this standard shall
be met when applicable and warranted by the intended installation and platform requirements.
Discussion: NDI refers to any equipment that is already developed and ready for use including
both commercial and military items. DoD SD-2 provides guidance on EMC integration issues
relating to the use of NDI. SD-2 states concerns with proper operation in the mission
environment and the need for compatibility with existing operational equipment. The document
includes cautions that acceptance in the commercial marketplace does not mean that EMC
requirements are met, that modifications to correct EMC problems can be costly and time
consuming, and that EMC problems can be potentially hazardous. SD-2 states that quantitative
EMC requirements should be developed and that valid data needs to be gathered during a market
investigation for performance of analysis to determine the suitability of the NDI. Testing may be
required if there is insufficient data. An EMC advisory board is recommended to provide
alternatives to decision makers.
It is common for the DoD to use commercially available medical devices onboard aeromedical
evacuation aircraft. This equipment needs to undergo a suitability assessment which involves
determining the environmental and EMI characteristics of the equipment for review by flight
certification personnel. A basic methodology has been established as described below for the
EMI portion of this assessment for Army and Air Force applications. Contractual compliance
with MIL-STD-461 is not imposed on the procurements. The MIL-STD-461 requirements that
are evaluated are CE102, CS101, CS114, CS115, CS116, RE102, and RS103 for both Services
and the addition of CE101 for the Army. Depending on whether aircraft power or battery
operation is used and the type of electrical interfaces, if any, will influence whether CE101,
CE102, CS101, CS114, CS115, and CS116 are necessary, as is the case with any equipment.
CS114 Curve 3 and the Air Force RS103 requirement of 20 V/m from 2 to 1000 MHz and 60
V/m levels from 1 to 18 GHz are treated as anticipated nominal performance levels.
Thresholding of any response is accomplished for these levels and the other susceptibility
evaluations. CS114 Curve 5 and 200 V/m measurements for RS103 are performed for severe
Army helicopter evaluations; however, the results are assessed using risk analysis oriented
toward patient safety, absolute performance is not expected and often does not result across the
frequency range of interest. Thresholding is not performed at these levels, only the results are
reported. Also, only the standard 1 kHz pulse modulation, 50 % duty cycle, specified in MIL-
STD-461 is used. The other types of modulation sometimes used by Army aviation are not
applied.
The US Army Aeromedical Research Lab (USAARL) at Fort Rucker, AL, is responsible for
airworthiness testing and certification of medical carry-on equipment for use on U.S. Army

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aircraft. Evaluation of emission results (aircraft safety issues) is the responsibility of the
Aviation Engineering Directorate at the U.S. Army Aviation and Missile, Research,
Development, and Engineering Center (AMRDEC), per Army Regulation (AR) 70-62.
Evaluation of the susceptibility results (patient safety issues) is the responsibility of USAARL
per Army Regulation (AR) 40-61. For the Air Force, Air Force Instruction (AFI) 11-202V3,
“General Flight Rules,” requires emissions testing of portable electronic devices to ensure
aircraft safety. ASC/EN, Wright-Patterson Air Force Base, OH, is responsible for equipment
certification related to these results. 77 AESG/TFL, Brooks City-Base, TX, is responsible for
assessing patient safety issues related to susceptibility results, with consultation with ASC/EN.
Since medical equipment often does not totally meet requirements, technical assessment of the
results determines if the equipment can be used without endangering the aircraft or unduly
affecting patient care. Aircraft level assessments are sometimes used to supplement the EMI
results. For example, the Army commonly assesses coupling to aircraft antennas on helicopters
to determine whether RE102 emissions above limits are degrading receivers.
A.4.2.4.1 (4.2.4.1) Commercial items (CI).
Discussion: The use of CI presents a dilemma between the need for EMI control with
appropriate design measures implemented and the desire to take advantage of existing designs
which may exhibit undesirable EMI characteristics. Paragraphs 4.2.4.1.1 and 4.2.4.1.2 address
the specific requirements for the two separate cases of contractor selection versus procuring
activity specification of commercial equipment.
For some applications of commercially developed products, such as commercial transport
aircraft, EMI requirements similar to those in this standard are usually imposed on equipment.
Most commercial aircraft equipment is required to meet the EMI requirements in RTCA DO-160
or an equivalent contractor in-house document. Recent revisions to RTCA DO-160 are making
the document more compatible with this standard. Equipment qualified to revisions C, D, or E
of RTCA DO-160 is often suitable for military aircraft applications.
EMI requirements on most commercial equipment are more varied and sometimes nonexistent.
The Federal Communication Commission (FCC) is responsible for regulating "Non-Licensed
Radio Frequency Devices" in the commercial and residential environment to control interference
to radio reception. Requirements are imposed in FCC CFR Title 47, Parts 2, 15, and 18. The
FCC does not control susceptibility (referred to as immunity in the commercial community)
characteristics of equipment. The most widely applied requirement is Part 15 which requires
that any "digital device" comply with the following conducted and radiated emission limits for
commercial environments (Class A) and residential environments (Class B).

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CONDUCTED EMISSIONS
FREQUENCY CLASS A CLASS B
(MHz) (dBμV) (dBμV)
0.45 - 1.705 60 48
1.705 – 30 70 48

RADIATED EMISSIONS
FREQUENCY CLASS A CLASS B
(MHz) (dBμV/m at 10 meters) (dBμV/m at 3 meters)
30 – 88 39 40
88 – 216 44 44
216 – 960 46 46
above 960 50 54
These requirements are typically less stringent than military requirements of a similar type.
Also, there is difficulty in comparing levels between commercial and military testing due to
differences in measurement distances, different types of antennas, and near-field conditions.
The commercial community is moving toward immunity standards. The basis for immunity
requirements is given in ANSI C63.12. There is also activity in the international area. The
European Union is imposing mandatory standards and the International Electrotechnic
Commission is working on standards.
A.4.2.4.1.1 (4.2.4.1.1) Selected by contractor.
When it is demonstrated that a commercial item selected by the contractor is responsible for
equipment or subsystems failing to meet the contractual EMI requirements, either the
commercial item shall be modified or replaced or interference suppression measures shall be
employed, so that the equipment or subsystems meet the contractual EMI requirements.
Discussion: The contractor retains responsibility for complying with EMI requirements
regardless of the contractor's choice of commercial off-the-shelf items. The contractor can treat
selected commercial items as necessary provided required performance is demonstrated.
A.4.2.4.1.2 (4.2.4.1.2) Specified by procuring activity.
When it is demonstrated by the contractor that a commercial item specified by the procuring
activity for use in an equipment or subsystem is responsible for failure of the equipment or
subsystem to meet its contractual EMI requirements, the data indicating such failure shall be
included in the Electromagnetic Interference Test Report (EMITR) (see 6.3). No modification or
replacement shall be made unless authorized by the procuring activity.
Discussion: The procuring activity retains responsibility for EMI characteristics of commercial
items that the procuring activity specifies to be used as part of a subsystem or equipment. The
procuring activity will typically study trade-offs between the potential for system-level problems

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and the benefits of retaining unmodified commercial equipment. The procuring activity needs to
provide specific contractual direction when modifications are considered to be necessary.
A.4.2.4.2. (4.2.4.2) Procurement of equipment or subsystems having met other EMI
requirements.
Procurement of equipment and subsystems electrically and mechanically identical to those
previously procured by activities of DoD or other Federal agencies, or their contractors, shall
meet the EMI requirements and associated limits, as applicable in the earlier procurement,
unless otherwise specified by the Command or agency concerned.
Discussion: In general, the government expects configuration controls to be exercised in the
manufacturing process of equipment and subsystems to ensure that produced items continue to
meet the particular EMI requirements to which the design was qualified. This standard reflects
the most up-to-date environments and concerns. Since the original EMI requirements may be
substantially different than those in this standard, they may not be adequate to assess the
suitability of the item in a particular installation. This situation most often occurs for equipment
susceptibility tests related to the radiated electromagnetic environment. Procuring activities
need to consider imposing additional test requirements on the contractor to gather additional data
to permit adequate evaluation.
Testing of production items has shown degraded performance of the equipment from that
previously demonstrated during development. One problem area is engineering changes
implemented for ease of manufacturing which are not adequately reviewed for potential effects
on EMI control design measures. Specific problems have been related to treatment of cable and
enclosure shields, electrical grounding and bonding, and substitution of new component parts
due to obsolescence.
A.4.2.5 (4.2.5) Government Furnished Equipment (GFE).
When it is demonstrated by the contractor that a GFE is responsible for failure of an equipment
or subsystem to meet its contractual EMI requirements, the data indicating such failure shall be
included in the EMITR. No modification shall be made unless authorized by the procuring
activity.
Discussion: GFE is treated the same as commercial items specified by the procuring activity.
A.4.2.6 (4.2.6) Switching transients.
Switching transient emissions that result at the moment of operation of manually actuated
switching functions are exempt from the requirements of this standard. Other transient type
conditions, such as automatic sequencing following initiation by a manual switching function,
shall meet the emissions requirements of this standard.
Discussion: Proper treatment of manually actuated switching functions has long been a
dilemma. Platform experience has shown that switching of electronics equipment subjected to
EMI requirements rarely causes electromagnetic compatibility problems. On this basis, there are
no requirements included in this standard. "On-off" switching has been of particular interest.
“On-off” switching has occasionally caused power quality type problems. These problems are
associated with voltage regulation difficulties from a large load being switched on a power bus;
however, such power quality issues are not addressed by this standard.

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APPENDIX A

Platform problems have also been observed from switching of items not normally subjected to
EMI requirements such as unsuppressed inductors (valves, relays, etc.), motors, and high current
resistive loads. These types of problems are more related to coupling of transients onto platform
wiring through electric and magnetic fields than direct conduction of the interference. There are
substantial requirements included in the standard to protect against susceptibility to transients.
This statement is not intended to imply that inductive devices and other transient producers
should not be suppressed as a normal good design practice. For example, some integrating
contractors routinely require vendors to provide diode suppression on inductors.
In earlier versions of EMI standards, manually actuated functions were measured using
frequency domain techniques. Although measured emission levels were often 40-70 dB above
the limit, no platform problems were observed. This technique was largely abandoned in later
versions of the standards in favor of a time domain requirement on power leads (CE07). Except
for some above limit conditions associated with on-off functions, equipment rarely have had any
problems with the requirement. Testing of on-off functions has often been controversial
because of the need to often use a switch external to the equipment. A number of issues arise
regarding placement of the switch, where the transient should be measured, whether the switch
or the equipment causes the transient, and whether the switch can be suppressed.
The exemption is applicable only for transient effects occurring at the moment of manual switch
operation. Many other transient type effects occur during the operation of electronics. An
argument could be made that the operation of microprocessor controlled electronics produces
continuous transients with every change of state. There are certain transient effects that occur
infrequently which could be presented to the procuring activity as events similar to the action of
a manual switch with a request for an exemption. An example is a heater circuit that functions
intermittently dependent upon a sensed temperature.
Other documents such as MIL-STD-704, MIL-STD-464, and MIL-STD-1399-300A impose
transient controls at the system-level.
A.4.2.7 (4.2.7) Interchangeable modular equipment.
The requirements of this standard are verified at the Shop Replaceable Unit, Line Replaceable
Unit, or Integrated Equipment Rack assembly level. When modular equipment such as line
replaceable modules are replaced or interchanged within the assembly additional testing or a
similarity assessment is required and shall be approved by the procuring activity.
Discussion: Different equipment with the same Form, Fit and Function characteristics may have
the potential for different EMI profiles, thus resulting in interchangeability issues. Additionally,
more subsystems and equipment are being designed and built by more than one manufacturer.
Different manufacturer’s unique designs such as filter placement on the motherboard or module,
general board design/circuit layout, compatibilities of Inputs/Outputs at higher frequencies,
component tolerances, board proximity, etc., will affect the electromagnetic interference
characteristics of the equipment. Therefore, testing of all possible configurations or a detailed
analysis assessing the design configuration changes is required.

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APPENDIX A

A.4.3 (4.3) Verification requirements.

The general requirements related to test procedures, test facilities, and equipment stated below,
together with the detailed test procedures included in 5, shall be used to determine compliance
with the applicable emission and susceptibility requirements of this standard. Any procuring
activity approved exceptions or deviations from these general requirements shall be documented
in the Electromagnetic Interference Test Procedures (EMITP) (see 6.3). Equipment that is
intended to be operated as a subsystem shall be tested as such to the applicable emission and
susceptibility requirements whenever practical. Formal testing is not to commence without
approval of the EMITP by the Command or agency concerned. Data gathered as a result of
performing tests in one electromagnetic discipline might be sufficient to satisfy requirements in
another. Therefore, to avoid unnecessary duplication, a single test program should be
established with tests for similar requirements conducted concurrently whenever possible.
Discussion: This portion of the document specifies general requirements that are applicable to a
variety of test procedures applicable for individual emissions and susceptibility requirements.
The detailed test procedures for each emissions and susceptibility requirement include
procedures that are unique to that requirement. Other sources of information dealing with
electromagnetic interference testing are available in industry documents such as RTCA DO-160
and SAE ARP 1972.
Electromagnetic disciplines [EMC, electromagnetic pulse (EMP), lightning, RF compatibility,
frequency allocation, etc.] are integrated to differing levels in various government and contractor
organizations. There is often a common base of requirements among the disciplines. It is more
efficient to have unified requirements and complete and concise testing. For example, the EMC,
EMP and lightning areas all pertain to electronic hardness to transients. The transient
requirements in this standard should satisfy most concerns or should be adapted as necessary to
do so.
Testing integrated equipment at the subsystem-level is advantageous because the actual electrical
interfaces are in place rather than electrical load or test equipment simulations. When
simulations are used, there is always doubt regarding the integrity of the simulation and
questions arise whether emission and susceptibility problems are due to the equipment under test
or the simulation.
Contractor generated test procedures provide a mechanism to interpret and adapt MIL-STD-461
as it is applicable to a particular subsystem or equipment and to detail the test agency's facilities
and instrumentation and their use. It is important that the procedures are available to the
procuring activity early so that the procuring activity can approve the test procedures prior to the
start of testing. Agreement needs to exist between the procuring activity and the contractor on
the interpretation of test requirements and procedures, thereby minimizing the possible need for
retesting.
When testing large equipment, equipment that requires special handling provision or high power
equipment, deviations from the standard testing procedures may be required. Large equipment
may not fit through the typical shielded room door or may be so heavy that it would crush the
floor. Other equipment has large movable arms or turrets or equipment that requires special
heating or cooling facilities. This equipment may have to be tested at the manufacturer’s
facilities or at the final installation. The following examples are for guidance. Sound

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APPENDIX A

engineering practices should be used and explained in detail in the EMITP when deviating from
the standard test procedures due to EUT characteristics. The design of the tests is of primary
importance and the data recorded during the testing must reflect the final installation
characteristics as closely as possible.
For equipment which requires high input current (for example: > 200 A), commercial LISNs
may not be available. Since LISNs are ineffective below 10 kHz, they may be deleted for CE101
testing. For CE102, the “voltage probe” called out in ANSI C63.4 may be substituted. The
construction of the probe is shown in Figure A-1. A direct connection to the power lines is
required and care must be taken to establish a reference ground for the measurements. It may be
necessary to perform repeated measurements over a suitable period of time to determine the
variation in the power line impedance and the impact on the measured emissions from the EUT.
The measurements are made between each current-carrying conductor in the supply mains and
the ground conductor with a blocking capacitor C and resistor R, as shown in Figure A-1, so that
the total resistance between the line under test and ground is 1500 ohm. The probe attenuates the
voltage so calibration factors are required. The measurement point (probe’s position on the
cables) must be identified in all test setups.
When equipment is too large or requires special provisions (loads, drives, water, emission of
toxic fumes and such), testing in a typical semi-anechoic room may not be feasible. Temporary
screen rooms consisting of hardware cloth can be built around the test area to reduce the ambient
for radiated emission testing and to contain the RF field during radiated susceptibility testing.
Since the room may be highly reflective, care must be taken to identify any resonances. Several
antenna positions may be required in order to reduce the effect of the resonances.
Equipment which produces high power RF output may be required to be tested on an open area
test site. Additionally, equipment that needs to have a communication link to the outside world
must be tested in the open. FCC approval may be required in order to generate the RF fields for
the RS103 test requirement. If the communication link can be simulated, then the test can be
performed in a shielded room. In this case, special dummy loads may be required, since the high
power RF radiation could damage the anechoic material due to heating.

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APPENDIX A

SUPPLY MAINS

C
XC < 1500 Ω

R = (1500 - RM) Ω

MEASUREMENT
RECEIVER

XL > RM INPUT IMPEDANCE = R M Ω

FIGURE A-1. Voltage probe for tests at user’s installation.

Imposition of EMI requirements on large equipment has become essential to prevent EMI
problems. Therefore, EMI requirements should not be waived simply because of special
handling problems or equipment size. Typical equipment and subsystems for which these
special provisions have been applied are as follows:
Air handling units (heating, ventilating, and air conditioning)
Large uninterruptible power supplies (UPS)
Equipment vans/motorized vehicles
Desalinization units
Large motors/generators/drives/power distribution systems
Large radars
Rail guns and their power sources
Catapults and their power sources
Multiple console subsystems

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APPENDIX A

A.4.3.1 (4.3.1) Measurement tolerances.

Unless otherwise stated for a particular measurement, the tolerance shall be as follows:
a. Distance: ±5%
b. Frequency: ±2%
c. Amplitude, measurement receiver: ±2 dB
d. Amplitude, measurement system (includes measurement receivers, transducers, cables,
and so forth): ±3 dB
e. Time (waveforms): ±5%
f. Resistors: ±5%
e. Capacitors: ±20%
Discussion: Tolerances are necessary to maintain reasonable controls for obtaining consistent
measurements. Paragraphs 4.3.1b through 4.3.1d are in agreement with ANSI C63.2 for
electromagnetic noise instrumentation.
A.4.3.2 (4.3.2) Shielded enclosures.
To prevent interaction between the EUT and the outside environment, shielded enclosures will
usually be required for testing. These enclosures prevent external environment signals from
contaminating emission measurements and susceptibility test signals from interfering with
electrical and electronic items in the vicinity of the test facility. Shielded enclosures must have
adequate attenuation such that the ambient requirements of 4.3.4 are satisfied. The enclosures
must be sufficiently large such that the EUT arrangement requirements of paragraph 4.3.8 and
antenna positioning requirements described in the individual test procedures are satisfied.
Discussion: Potential accuracy problems introduced by shielded enclosure resonances are well
documented and recognized; however, shielded enclosures are usually a necessity for testing of
military equipment to the requirements of this standard. Most test agencies are at locations
where ambient levels outside of the enclosures are significantly above the limits in this standard
and would interfere with the ability to obtain meaningful data.
Electrical interfaces with military equipment are often complex and require sophisticated test
equipment to simulate and evaluate the interface. This equipment usually must be located
outside of the shielded enclosure to achieve sufficient isolation and prevent it from
contaminating the ambient and responding to susceptibility signals.
The shielded enclosure also prevents radiation of applied susceptibility signals from interfering
with local antenna-connected receivers. The most obvious potential offender is the RS103 test.
However, other susceptibility tests can result in substantial radiated energy that may violate
Federal Communication Commission (FCC) rules.

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APPENDIX A

A.4.3.2.1 (4.3.2.1) Radio Frequency (RF) absorber material.

RF absorber material (carbon impregnated foam pyramids, ferrite tiles, and so forth) shall be
used when performing electric field radiated emissions or radiated susceptibility testing inside a
shielded enclosure to reduce reflections of electromagnetic energy and to improve accuracy and
repeatability. The RF absorber shall be placed above, behind, and on both sides of the EUT,
and behind the radiating or receiving antenna as shown in Figure 1. Minimum performance of
the material shall be as specified in Table I. The manufacturer's certification of their RF
absorber material (basic material only, not installed) is acceptable.
TABLE I. Absorption at normal incidence.

Frequency Minimum absorption

80 MHz - 250 MHz 6 dB
above 250 MHz 10 dB

DISCUSSION: Accuracy problems with making measurements in untreated shielded enclosures

due to reflections of electromagnetic energy have been widely recognized and documented. The
values of RF absorption required by Table I are considered to be sufficient to substantially
improve the integrity of the measurements without unduly impacting test facilities. The
minimum placement provisions for the material are specified to handle the predominant
reflections. The use of additional material is desirable, where possible. It is intended that the
values in Table I can be met with available ferrite tile material or standard 24 inch (0.61 meters)
pyramidal absorber material.
A.4.3.3 (4.3.3) Other test sites.
If other test sites are used, the ambient requirements of paragraph 4.3.4 shall be met.
Discussion: For certain types of EUTs, testing in a shielded enclosure may not be practical.
Examples are EUTs which are extremely large, require high electrical power levels or motor
drives to function, emit toxic fumes, or are too heavy for normal floor loading (see A.4.3
discussion for additional information). There is a serious concern with ambient levels
contaminating data when testing is performed outside of a shielded enclosure. Therefore, special
attention is given to this testing under 4.3.4, "Ambient electromagnetic level." All cases where
testing is performed outside a shielded enclosure shall be justified in detail in the EMITP,
including typical profiles of expected ambient levels.
If it is necessary to operate EUTs that include RF transmitters outside of a shielded enclosure,
spectrum certification and a frequency assignment must first be obtained through the spectrum
management process.
An option in emission testing is the use of an open area test site (OATS) in accordance with
ANSI C63.4. These sites are specifically designed to enhance accuracy and repeatability. Due
to differences between ANSI C63.4 and this standard in areas such as antenna selection,
measurement distances, and specified frequency ranges, the EMITP shall detail the techniques
for using the OATS and relating the test results to the requirements of this standard.

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A.4.3.4 (4.3.4) Ambient electromagnetic level.

During testing, the ambient electromagnetic level measured with the EUT de-energized and all
auxiliary equipment turned on shall be at least 6 dB below the allowable specified limits when
the tests are performed in a shielded enclosure. Ambient conducted levels on power leads shall
be measured with the leads disconnected from the EUT and connected to a resistive load which
draws the same rated current as the EUT. When tests are performed in a shielded enclosure and
the EUT is in compliance with required limits, the ambient profile need not be recorded in the
EMITR. When measurements are made outside a shielded enclosure, the tests shall be
performed during times and conditions when the ambient is at its lowest level. The ambient shall
be recorded in the EMITR and shall not compromise the test results.
Discussion: Controlling ambient levels is critical to maintaining the integrity of the gathered
data. High ambients present difficulties distinguishing between EUT emissions and ambient
levels. Even when specific signals are known to be ambient related, they may mask EUT
emissions that are above the limits of this standard.
The requirement that the ambient be at least 6 dB below the limit ensures that the combination of
the EUT emissions and ambient does not unduly affect the indicated magnitude of the emission.
If a sinusoidal noise signal is at the limit and the ambient is 6 dB below the limit, the indicated
level would be approximately 3 dB above the limit. Similarly, if the ambient were allowed to be
equal to the limit for the same true emission level, the indicated level would be approximately
5 dB above the limit.
A resistive load is specified to be used for conducted ambients on power leads. However, under
certain conditions actual ambient levels may be higher than indicated with a resistive load. The
most likely reason is the presence of capacitance at the power interface of the EUT that will
lower the input impedance at higher frequencies and increase the current. This capacitance
should be determined and ambient measurements repeated with the capacitance in place. There
is also the possibility of resonance conditions with shielded room filtering, EUT filtering, and
power line inductance. These types of conditions may need to be investigated if unexpected
emission levels are observed.
Testing outside of a shielded enclosure often must be performed at night to minimize influences
of the ambient. A prevalent problem with the ambient is that it continuously changes with time
as various emitters are turned on and off and as amplitudes fluctuate. A useful tool for
improving the flow of testing is to thoroughly analyze the EUT circuitry prior to testing and
identify frequencies where emissions may be expected to be present.
An option to improve overall measurement accuracy is to make preliminary measurements inside
a shielded enclosure and accurately determine frequencies where emissions are present. Testing
can be continued outside the shielded enclosure with measurements being repeated at the
selected frequencies. The 6 dB margin between the ambient and limits must then be observed
only at the selected frequencies.
A.4.3.5 (4.3.5) Ground plane.
The EUT shall be installed on a ground plane that simulates the actual installation. If the actual
installation is unknown or multiple installations are expected, then a metallic ground plane shall
be used. Unless otherwise specified below, ground planes shall be 2.25 square meters or larger

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APPENDIX A

in area with the smaller side no less than 76 cm. When a ground plane is not present in the EUT
installation, the EUT shall be placed on a non-conductive table.
Discussion: Generally, the radiated emissions and radiated susceptibilities of equipment are due
to coupling from and to the interconnecting cables and not via the case of the EUT. Emissions
and susceptibility levels are directly related to the placement of the cable with respect to the
ground plane and to the electrical conductivity of the ground plane. Thus, the ground plane
plays an important role in obtaining the most realistic test results.
When the EUT is too large to be installed on a conventional ground plane on a bench, the actual
installation should be duplicated. For example, a large radar antenna may need to be installed on
a test stand and the test stand bonded to the floor of the shielded enclosure. Ground planes need
to be placed on the floor of shielded rooms with floor surfaces such as tiles that are not
electrically conductive.
The use of ground planes is also applicable for testing outside of a shielded enclosure. These
ground planes will need to be referenced to earth as necessary to meet the electrical safety
requirements of the National Electrical Code. Where possible, these ground planes should be
electrically bonded to other accessible grounded reference surfaces such as the outside structure
of a shielded enclosure.
The minimum dimensions for a ground plane of 2.25 square meters with 76 cm on the smallest
side will be adequate only for setups involving a limited number of EUT enclosures with few
electrical interfaces. The ground plane must be large enough to allow for the requirements
included in paragraph 4.3.8 on positioning and arrangement of the EUT and associated cables to
be met.
A.4.3.5.1 (4.3.5.1) Metallic ground plane.
When the EUT is installed on a metallic ground plane, the ground plane shall have a surface
resistance no greater than 0.1 milliohms per square. The DC resistance between metallic
ground planes and the shielded enclosure shall be 2.5 milliohms or less. The metallic ground
planes shown in Figures 2 through 5 shall be electrically bonded to the floor or wall of the basic
shielded room structure at least once every 1 meter. The metallic bond straps shall be solid and
maintain a five-to-one ratio or less in length to width. Metallic ground planes used outside a
shielded enclosure shall extend at least 1.5 meters beyond the test setup boundary in each
direction.
Discussion: For the metallic ground plane, a copper ground plane with a thickness of 0.25
millimeters has been commonly used and satisfies the surface resistance requirements. Other
metallic materials of the proper size and thickness needed to achieve the resistivity can be
substituted.
For metallic ground planes, the surface resistance can be calculated by dividing the bulk
resistivity by the thickness. For example, copper has a bulk resistivity of 1.75x10-8 ohm-meters.
For a 0.25 millimeter thick ground plane as noted above, the surface resistance is
1.7x10-8/2.5x10-4 = 6.8x10-5 ohms per square = 0.068 milliohms per square. The requirement is
0.1 milliohms per square.

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APPENDIX A

A.4.3.5.2 (4.3.5.2) Composite ground plane.

When the EUT is installed on a conductive composite ground plane, the surface resistivity of the
typical installation shall be used. Composite ground planes shall be electrically bonded to the
enclosure with means suitable to the material.
Discussion: A copper ground plane has typically been used for all testing in the past. For most
instances, this has been adequate. However, with the increasing use of composites, the
appropriate ground plane will play a bigger role in the test results. Limited testing on both
copper and conductive composite ground planes has shown some differences in electromagnetic
coupling test results, thus the need exists to duplicate the actual installation, if possible. In some
cases, it may be necessary to include several ground planes in the same test setup if different
units of the same EUT are installed on different materials in the installation.
With the numerous different composite materials being used in installations, it is not possible to
specify a general resistivity value. The typical resistivity of carbon composite is about 2000
times that of aluminum. The actual resistivity needs to be obtained from the installation
contractor and used for testing.
A.4.3.6 (4.3.6) Power source impedance.
The impedance of power sources providing input power to the EUT shall be controlled by Line
Impedance Stabilization Networks (LISNs) for all measurement procedures of this document
unless otherwise stated in a particular test procedure. LISNs shall not be used on output power
leads. The LISNs shall be located at the power source end of the exposed length of power leads
specified in paragraph 4.3.8.6.2. The LISN circuit shall be in accordance with the schematic
shown in Figure 6. The LISN impedance characteristics shall be in accordance with Figure 7.
The LISN impedance shall be measured at least annually under the following conditions:
a. The impedance shall be measured between the power output lead on the load side of the
LISN and the metal enclosure of the LISN.
b. The signal output port of the LISN shall be terminated in fifty ohms.
c. The power input terminal on the power source side of the LISN shall be unterminated.
The impedance measurement results shall be provided in the EMITR.
Discussion: The impedance is standardized to represent expected impedances in actual
installations and to ensure consistent results between different test agencies. Versions of MIL-
STD-462 (previously contained test procedures for MIL-STD-461 requirements) in the past used
10 μF feedthrough capacitors on the power leads. The intent of these devices was to determine
the current generator portion of a Norton current source model. If the impedance of the
interference source was also known, the interference potential of the source could be analytically
determined for particular circumstances in the installation. A requirement was never established
for measuring the impedance portion of the source model. More importantly, concerns arose
over the test configuration influencing the design of power line filtering. Optimized filters are
designed based on knowledge of both source and load impedances. Significantly different filter
designs will result for the 10 μF capacitor loading versus the impedance loading shown in
Figure 7 of the main body.

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LISNs are not used on output power leads. Emission measurements using LISNs are performed
on input power leads because the EUT is using a power source common to many other
equipment items and the EUT must not degrade the quality of the power. When the EUT is the
source of power, the issue is completely different since the electrical characteristics of the power
required are controlled by the defined power quality requirements. Output power leads should
be terminated with appropriate electrical loading that produces potentially worst case emission
and susceptibility characteristics.
The particular configuration of the LISN is specified for several reasons. A number of
experiments were performed to evaluate typical power line impedances present in a shielded
room on various power input types both with and without power line filters and to assess the
possible methods of controlling the impedance. An approach was considered for the standard to
simply specify an impedance curve from 30 Hz to 100 MHz and to allow the test agency to meet
the impedance using whatever means the agency found suitable. The experiments showed that
there were no straightforward techniques to maintain desired controls over the entire frequency
range.
A specific 50 μH LISN (see ANSI C63.4) was selected to maintain a standardized control on the
impedance as low as 10 kHz. Five μH LISNs used commonly in the past provide little control
below 100 kHz. Impedance control below 10 kHz is difficult. From evaluations of several 50
μH LISN configurations, the one specified demonstrated the best overall performance for various
shielded room filtering variations. Near 10 kHz, the reactances of the 50 μH inductor and 8 μF
capacitor cancel and the LISN is effectively a 5 ohm resistive load across the power line.
Using a common LISN is important for standardization reasons. However, the use of alternative
LISNs may be desirable in certain application where the characteristics of the LISN may not be
representative of the actual installation and the design of EUT circuitry is being adversely
affected. For example, there are issues with switching power supply stability and the power
source impedance seen by the power supply. The 50 μH inductor in the LISN represents the
inductance of power distribution wiring running for approximately 50 meters. For a large
platform, such as a ship or cargo aircraft, this value is quite representative of the actual
installation. However, for smaller platforms such as fighter aircraft, inductance values may be
substantially lower than 50 μH. If alternative LISN designs are used, certain issues need to be
addressed such as the frequency range over which effective impedance control is present and
where voltage versus current measurements are appropriate.
Caution needs to be exercised in using the LISN for 400 Hz power systems. Some existing
LISNs may not have components sufficient to handle the power dissipation requirements. At
115 volts, 400 Hz, the 8 μF capacitor and 5 ohm resistor will pass approximately 2.3 amperes
which results in 26.5 watts being dissipated in the resistor.
Under CE101 and CE102 discussions, the use of a 5 μH LISN is suggested as a possible
alternative under certain circumstances. Figures A-2 and A-3 below show design and impedance
characteristics of an appropriate LISN. Refer to those sections in this appendix for further
details.

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FIGURE A-2. 5 μH LISN schematic.

60

tolerance on impedance is +/-20%

50

40
Imepdance Ω

30

20

10

0
0.1 1 10 100
Frequency MHz

FIGURE A-3. 5 μH LISN impedance.

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A.4.3.7 (4.3.7) General test precautions.

Discussion: The requirements included in paragraph 4.3.7 cover important areas related to
improving test integrity and safety that need special attention. There are many other areas where
test difficulties may develop. Some are described here.
It is common for shields to become loose or broken at connectors on coaxial cables resulting in
incorrect readings. There also are cases where center conductors of coaxial cables break or
separate. Periodic tests should be performed to ensure cable integrity. Special low loss cables
may be required when testing at higher frequencies.
Caution needs to be exercised when performing emission testing at frequencies below
approximately 10 kHz to avoid ground loops in the instrumentation which may introduce faulty
readings. A single-point ground often needs to be maintained. It is usually necessary to use
isolation transformers at the measurement receiver and accessory equipment. The single-point
ground is normally established at the access (feedthrough) panel for the shielded enclosure.
However, if a transducer is being used which requires an electrical bond to the enclosure (such
as the rod antenna counterpoise), the coaxial cable will need to be routed through the enclosure
access panel without being grounded. Since the shielded room integrity will then be
compromised, a normal multiple point grounded setup needs to be re-established as low in
frequency as possible.
Rather than routing the coaxial cable through the enclosure access panel without grounding it to
the enclosure, a 50-ohm video isolation transformer may be connected to the grounded RF
connector at the access panel inside the room. Normal connection of the measuring receiver is
made to the grounded connector at the panel outside the room. This technique effectively breaks
the ground loop without sacrificing the room's shielding integrity. The losses of the video
isolation transformer must be accounted for in the measurement data. These devices are
typically useful up to approximately 10 MHz.
If isolation transformers are found to be necessary in certain setups, problems may exist with
items powered by switching power supplies. A solution is to use transformers that are rated at
approximately five times the current rating of the item.
Solid state instrumentation power sources have been found to be susceptible to radiated fields
even to the extent of being shut down. It is best to keep these items outside of the shielded
enclosure.
A.4.3.7.1 (4.3.7.1) Accessory equipment.
Accessory equipment used in conjunction with measurement receivers shall not degrade
measurement integrity.
Discussion: Measurement receivers are generally designed to meet the limits of this standard so
they do not contaminate the ambient for emission testing when they are used inside the shielded
enclosure. However, accessory equipment such as computers, oscilloscopes, plotters, or other
instruments used to control the receiver or monitor its outputs can cause problems. They may
compromise the integrity of the receiver by radiating signals conducted out of the receiver from
improperly treated electrical interfaces or may produce interference themselves and raise the
ambient. Even passive devices such as headsets have been known to impact the test results.

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It is best to locate all of the test equipment outside of the shielded enclosure with the obvious
exception of the transducer (antenna or current probe). Proper equipment location will ensure
that the emissions being measured are being generated in the EUT only and will help ensure that
the ambient requirements of 4.3.4 are met. If the equipment must be used inside the enclosure or
if testing is being conducted outside of an enclosure, the measurement receiver and accessory
equipment should be located as far away from the transducers as practical to minimize any
impact.
A.4.3.7.2 (4.3.7.2) Excess personnel and equipment.
The test area shall be kept free of unnecessary personnel, equipment, cable racks, and desks.
Only the equipment essential to the test being performed shall be in the test area or enclosure.
Only personnel actively involved in the test shall be permitted in the enclosure.
Discussion: Excess personnel and both electronic and mechanical equipment such as desks or
cable racks in the enclosure can affect the test results. During radiated emission testing in
particular, all nonessential personnel and equipment should be removed from the test site. Any
object in the enclosure can significantly influence or introduce standing waves in the enclosure
and thus alter the test results. The requirement to use RF absorber material will help to mitigate
these effects. However, material performance is not defined below 80 MHz for practical reasons
and standing waves continue to be a concern.
A.4.3.7.3 (4.3.7.3) Overload precautions.
Measurement receivers and transducers are subject to overload, especially receivers without
preselectors and active transducers. Periodic checks shall be performed to assure that an
overload condition does not exist. Instrumentation changes shall be implemented to correct any
overload condition.
Discussion: Overloads can easily go unnoticed if there is not an awareness of the possibility of
an overload or active monitoring for the condition. The usual result is a leveling of the output
indication of the receiver.
Two types of overloads are possible. A narrowband signal such as a sinusoid can saturate any
receiver or active transducer. Typical procedures for selecting attenuation settings for
measurement receivers place detected voltages corresponding to emission limits well within the
dynamic range of the receiver. Saturation problems for narrowband type signals will normally
only appear for a properly configured receiver if emissions are significantly above the limits.
Saturation can occur more readily when receivers are used to monitor susceptibility signals due
to the larger voltages involved.
Overload from impulsive type signals with broad frequency content can be much more
deceptive. This condition is most likely to occur with devices without a tunable bandpass feature
in the first stage of the signal input. Examples are preamplified rod antennas and spectrum
analyzers without preselectors. The input circuitry is exposed to energy over a large portion of
the frequency spectrum. Preselectors include a tunable tracking filter which bandwidth limits the
energy applied to the receiver front end circuitry.
Measurement receiver overload to both narrowband and impulsive type signals can be evaluated
by applying a 10 dB additional attenuation in the first stage of the receiver (before mixer

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circuitry) or external to the receiver. If overload is not present, the observed output will
uniformly decrease by 10 dB.
Overload conditions for active antennas are normally published as part of the literature supplied
with the antenna. For narrowband signals, the indicated level in the data can be reviewed with
respect to the literature to evaluate overload. Levels are also published for impulsive type
signals; however, these levels are not very useful since they usually assume that a flat field exists
across the useable range of the antenna. In reality, the impulsive field will vary significantly
with frequency and the antenna circuitry sees the integration of the spectral content of this field
over its bandpass. The primary active antenna used is an active rod antenna. Overload can be
evaluated by collapsing the rod and observing the change in indication. If overload is not
present, the indicated level should drop approximately 8 dB (rod at 30% of its original height).
The actual change for any particular manufacturer's product will depend on the telescoping
design and can be determined by radiating a signal to the antenna that is within its linear range.
A.4.3.7.4 (4.3.7.4) RF hazards.
Some tests in this standard will result in electromagnetic fields that are potentially dangerous to
personnel. The permissible exposure levels in DoDI 6055.11 shall not be exceeded in areas
where personnel are present. Safety procedures and devices shall be used to prevent accidental
exposure of personnel to RF hazards.
Discussion: During some radiated susceptibility and radiated emission testing, RS103, RS105
and RE103 in particular, fields may exceed the permissible exposure levels in DoDI 6055.11.
During these tests, precautions must be implemented to avoid inadvertent exposure of personnel.
Monitoring of the EUT during testing may require special techniques such as remotely
connected displays external to the enclosure or closed circuit television to adequately protect
personnel.
A.4.3.7.5 (4.3.7.5) Shock hazard.
Some of the tests require potentially hazardous voltages to be present. Extreme caution must be
taken by all personnel to assure that all safety precautions are observed.
Discussion: A safety plan and training of test personnel are normally required to assure that
accidents are minimized. Test equipment manufacturers' precautions need to be followed, if
specified. If these are not available, the test laboratory should establish adequate safety
precautions and train all test personnel. Special attention should be observed for CS109 since
electronic enclosures are intentionally isolated from the ground plane for test purposes.
A.4.3.7.6 (4.3.7.6) Federal Communications Commission (FCC) restrictions.
Some of the tests require high level signals to be generated that could interfere with normal FCC
approved frequency assignments. All such testing should be conducted in a shielded enclosure.
Some open site testing may be feasible if prior FCC coordination is accomplished.
Discussion: Radiated susceptibility RS103 testing and possibly other tests will produce signals
above FCC authorizations. This situation is one of the reasons that shielded enclosures are
normally required.

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A.4.3.8 (4.3.8) EUT test configurations.

The EUT shall be configured as shown in the general test setups of Figures 1 through 5 as
applicable. These setups shall be maintained during all testing unless other direction is given
for a particular test procedure.
Discussion: Emphasis is placed on "maintaining" the specified setup for all testing unless a
particular test procedure directs otherwise. Confusion has resulted from previous versions of the
standard regarding consistency of setups between individual requirements in areas such as lead
lengths and placement of 10 μF capacitors on power leads. In this version of the standard, any
changes from the general test setup are specifically stated in the individual test procedure.
A.4.3.8.1 (4.3.8.1) EUT design status.
EUT hardware and software shall be representative of production. Software may be
supplemented with additional code that provides diagnostic capability to assess performance.
Discussion: It is important that the hardware and software being tested is the same as the
equipment that is being fielded. Sometimes equipment is tested which is pre-production and
contains circuit boards that do not include the final layout or software that is not the final
version. Questions inevitably arise concerning the effects of the differences between the tested
equipment and production configurations on the qualification status of the equipment.
Analytically determining the impact is usually difficult.
A.4.3.8.2 (4.3.8.2) Bonding of EUT.
Only the provisions included in the design of the EUT shall be used to bond units such as
equipment case and mounting bases together, or to the ground plane. When bonding straps are
required, they shall be identical to those specified in the installation drawings.
Discussion: Electrical bonding provisions for equipment are an important aspect of platform
installation design. Adequacy of bonding is usually one of the first areas reviewed when
platform problems develop. Electrical bonding controls common mode voltages that develop
between the equipment enclosures and the ground plane. Voltages potentially affecting the
equipment will appear across the bonding interface when RF stresses are applied during
susceptibility testing. Voltages will also develop due to internal circuit operation and will
contribute to radiated emission profiles. Therefore, it is important that the test setup use actual
bonding provisions so that test results are representative of the intended installation.
A.4.3.8.3 (4.3.8.3) Shock and vibration isolators.
EUTs shall be secured to mounting bases having shock or vibration isolators if such mounting
bases are used in the installation. The bonding straps furnished with the mounting base shall be
connected to the ground plane. When mounting bases do not have bonding straps, bonding
straps shall not be used in the test setup.
Discussion: Including shock and vibration isolators in the setup when they represent the
platform installation is important. The discussion above for 4.3.8.2 is also applicable to shock
and vibration isolators; however, the potential effect on test results is even greater. Hard
mounting of the equipment enclosures to the ground plane can produce a low impedance path
across the bonding interface over most of the frequency range of interest. The bonding straps
associated with isolators will typically represent significant impedances at frequencies as low as
tens of kilohertz. The common mode voltages associated with these impedances will generally

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be greater than the hard mounted situation. Therefore, the influence on test results can be
substantial.
A.4.3.8.4 (4.3.8.4) Safety grounds.
When external terminals, connector pins, or equipment grounding conductors are available for
safety ground connections and are used in the actual installation, they shall be connected to the
ground plane. Arrangement and length shall be in accordance with 4.3.8.6.1. Shorter lengths
shall be used if they are specified in the installation instructions.
Discussion: Safety grounds used in equipment enclosures have been the source of problems
during EMI testing. Since they are connected to the equipment enclosure, they would be
expected to be at a very low potential with respect to the ground plane and a non-contributor to
test results. However, the wire lengths within enclosures are often sufficiently long that coupling
to them results from noisy circuits. Also, safety grounds can conduct induced signals from
external sources and reradiate within the equipment enclosure. Therefore, they must be treated
similarly to other wiring.
A.4.3.8.5 (4.3.8.5) Orientation of EUTs.
EUTs shall be oriented such that surfaces which produce maximum radiated emissions and
respond most readily to radiated signals face the measurement antennas. Bench mounted EUTs
shall be located 10 ±2 cm from the front edge of the ground plane subject to allowances for
providing adequate room for cable arrangement as specified below.
Discussion: Determination of appropriate surfaces is usually straightforward. Seams on
enclosures that have metal-to-metal contact or contain EMI gaskets rarely contribute and should
be considered low priority items. Prime candidates are displays such as video screens,
ventilation openings, and cable penetrations. In some cases, it may be necessary to probe the
surfaces with a sensor and measurement receiver to decide on EUT orientation.
MIL-STD-462 (superseded by this standard) specifically required probing with a loop antenna to
determine localized areas producing maximum emissions or susceptibility for radiated electric
field testing. The test antennas were to be placed one meter from the identified areas. The
requirement was not included in this standard due to difficulties in applying the requirement and
the result that probing was often not performed. Probing implies both scanning in frequency and
physical movement of the probe. These two actions cannot be performed in a manner to cover
all physical locations at all frequencies. A complete frequency scan can be performed at
particular probe locations and movement of the probe over the entire test setup can be performed
at particular frequencies. The detailed requirements on the use of multiple antenna positions and
specific requirements on the placement of the antennas in test procedures for RE102 and RS103
minimize concerns with the need to probe.
A.4.3.8.6 (4.3.8.6) Construction and arrangement of EUT cables.
Electrical cable assemblies shall simulate actual installation and usage. Shielded cables or
shielded leads within cables shall be used only if they have been specified in installation
requirements. Input (primary) power leads, returns, and wire grounds shall not be shielded.
Cables shall be checked against installation requirements to verify proper construction
techniques such as use of twisted pairs, shielding, and shield terminations. Details on the cable
construction used for testing shall be included in the EMITP.

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Discussion: For most EUTs, electrical interface requirements are covered in interface control or
similar documents. Coordination between equipment manufacturers and system integration
organizations is necessary to ensure a compatible installation from both functional and
electromagnetic interference standpoints. For general purpose EUTs, which may be used in
many different installations, either the equipment specifications cover the interface requirements
or the manufacturers publish recommendations in the documentation associated with the
equipment.
Equipment manufacturers sometimes contend that failures during EMI testing are not due to their
equipment and can be cured simply by placing overall shields on the interface cabling. High
level emissions are often caused by electronic circuits within EUT enclosures coupling onto
cables simulating the installation which interface with the EUT. Overall shielding of the cabling
is certainly permissible if it is present in the installation. However, the use of overall shielding
that is not representative of the installation would result in test data that is useless. Also, overall
shielding of cabling in some installations is not a feasible option due to weight and maintenance
penalties. The presence of platform structure between cabling and antennas on a platform is not
an acceptable reason for using overall shields on cables for testing in accordance with this
standard. The presence of some platform shielding is a basic assumption.
An issue that arises with power leads concerns the use of shielding. It is unusual for power leads
to be shielded in the actual installation. If they come directly off a prime power bus, shielding
can only be effective if the entire bus is shielded end-to-end. Since buses normally distribute
power to many locations, it is not practical to shield them. An exception to this situation is when
power is derived from an intermediate source that contains filtering. Shielding between the
intermediate source and the EUT will then be effective. When it is proposed that shielded power
leads be used in the test setup, the configuration needs to be researched to ensure that it is
correct. There may be instances when published interface information is not available. In this
case, overall shielding is not to be used. Individual circuits are to be treated as they typically
would for that type of interface with shielding not used in questionable cases.
For some testing performed in the past using bulk cable drive techniques, overall cable shields
were routinely removed and the injected signal was applied to the core wiring within the shield.
The intent of this standard is to test cables as they are configured in the installation. If the cable
uses an overall shield, the test signal is applied to the overall shielded cable. If the procuring
agency desires that the test be performed on the core wiring, specific wording needs to be
included in contractual documentation.
In some instances, Navy surface ship applications specify shielded power leads for a particular
length of run. The shielded arrangement may be simulated in the test setup. Since unshielded
power distribution wiring will be present at some point in the installation, an additional length of
unshielded power leads (not less than 2 meters) should normally be added and routed parallel to
the front plane of the test setup boundary during radiated testing. Approval of the procuring
activity is required for using power leads that are entirely shielded. The additional unshielded
cable should not be used during conducted emissions testing.
A.4.3.8.6.1 (4.3.8.6.1) Interconnecting leads and cables.
Individual leads shall be grouped into cables in the same manner as in the actual installation.
Total interconnecting cable lengths in the setup shall be the same as in the actual platform

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installation. If a cable is longer than 10 meters, at least 10 meters shall be included. When
cable lengths are not specified for the installation, cables shall be sufficiently long to satisfy the
conditions specified below. At least the first 2 meters (except for cables which are shorter in the
actual installation) of each interconnecting cable associated with each enclosure of the EUT
shall be run parallel to the front boundary of the setup. Remaining cable lengths shall be routed
to the back of the setup and shall be placed in a zig-zagged arrangement. When the setup
includes more than one cable, individual cables shall be separated by 2 cm measured from their
outer circumference. For bench top setups using ground planes, the cable closest to the front
boundary shall be placed 10 cm from the front edge of the ground plane. All cables shall be
supported 5 cm above the ground plane.
Discussion: Actual lengths of cables used in installations are necessary for several reasons. At
frequencies below resonance, coupling is generally proportional to cable length. Resonance
conditions will be representative of the actual installation. Also, distortion and attenuation of
intentional signals due strictly to cable characteristics will be present and potential susceptibility
of interface circuits to induced signals will therefore be similar to the actual installation.
Zig-zagging of long cables is accomplished by first placing a length of cable in an open area and
then reversing the direction of the cable run by 180 degrees each time a change of direction is
required. Each subsequent segment is farther from the first. Individual segments of the cable are
parallel and should be kept 2 cm apart. The zig-zagging of long cables rather than coiling is to
control excess inductance. A 2 cm spacing between cables is required to expose all cabling to
the test antennas and limit coupling of signals between cables. The 10 cm dimension for cables
from the front edge of the ground plane ensures that there is sufficient ground plane surface
below the first cable to be effective. The 5 cm standoffs standardize loop areas available for
coupling and capacitance to the ground plane. The standoffs represent routing and clamping of
cables in actual installations a fixed distance from structure.
The requirement that the first 2 meters of each interconnecting cable associated with each
enclosure of the EUT be routed parallel to the front boundary of the setup is intended to ensure
that radiated emissions and susceptibility testing properly assesses the performance of the EUT.
Noise signals developed within the EUT and conducted outside on electrical interfaces will tend
to be attenuated as they travel along interconnecting cables, particularly at frequencies where the
associated wavelength is becoming short compared with the cable length. Similarly, induced
signals on interconnecting cables from radiated susceptibility fields will be attenuated as they
travel along the cable. Requiring that the first 2 meters of the cabling be exposed therefore
maximizes the effects of potential radiated coupling.
In some military applications, there can be over 2000 cables associated with a subsystem. In
most cases where large numbers of cables are involved, there will be many identical cable
interfaces connected to identical circuitry. Testing of every cable interface is not necessary in
this situation. The EMITP should document instances where these circumstances exist and
should propose which cables are to be included in the setup and to be tested.
A.4.3.8.6.2 (4.3.8.6.2) Input (primary) power leads.
Two meters of input power leads (including neutrals and returns) shall be routed parallel to the
front edge of the setup in the same manner as the interconnecting leads. Each input power lead,
including neutrals and returns, shall be connected to a LISN (see 4.3.6). Power leads that are

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bundled as part of an interconnecting cable in the actual installation shall be separated from the
bundle and routed to the LISNs (outside the shield of shielded cables). After the 2 meter exposed
length, the power leads shall be terminated at the LISNs in as short a distance as possible. The
total length of power lead from the EUT electrical connector to the LISNs shall not exceed
2.5 meters. All power leads shall be supported 5 cm above the ground plane. If the power leads
are twisted in the actual installation, they shall be twisted up to the LISNs.
Discussion: Appropriate power lead length is a trade-off between ensuring sufficient length for
efficient coupling of radiated signals and maintaining the impedance of the LISNs. To keep a
constant setup, it is undesirable to change the power lead length for different test procedures.
Requiring a 2 meter exposed length is consistent with treatment of interconnecting leads for
radiated concerns. Wiring inductance 5 cm from a ground plane is approximately 1 μH/m. At
1 MHz this inductance has an impedance of approximately 13 ohms which is significant with
respect to the LISN requirement.
While it is common to require that neutrals and returns be isolated from equipment chassis
within equipment enclosures, there are some cases where the neutral or return is tied directly to
chassis. If the equipment is electrically bonded to metallic system structure in the installation and
the system power source neutral or return is also tied to system structure, power return currents
will flow primarily through system structure rather than through wiring. For this case, a LISN
should normally be used only on the high side of the power. There are other installations, such
as many types of aircraft, where returns and neutrals are isolated within the equipment, but they
are often connected to system structure outside of the equipment enclosure. This practice allows
for the flexibility of using a wired return, if necessary. For this situation, LISNs should normally
be used on neutrals and returns to test for the wired return configuration.
The LISN requirement standardizes impedance for power leads. While signal and control
circuits are usually terminated in specified impedances, power circuit impedances are not usually
well defined. The LISN requirement applies to all input prime power leads. The LISN
requirement does not apply to output power leads. These leads should be terminated after the 2
meter exposed length in a load representing worst-case conditions. This load would normally
draw the maximum current allowed for the power source.
The construction of the power cable between the EUT and the LISNs must be in accordance with
the requirements of 4.3.8.6. For example, if a twisted triplet is used to distribute three phase
ungrounded power in the actual installation, the same construction should be used in the test
setup. The normal construction must be interrupted over a sufficient length to permit connection
to the LISNs.
A.4.3.8.7 (4.3.8.7) Electrical and mechanical interfaces.
All electrical input and output interfaces shall be terminated with either the actual equipment
from the platform installation or loads which simulate the electrical properties (impedance,
grounding, balance, and so forth) present in the actual installation. Signal inputs shall be
applied to all applicable electrical interfaces to exercise EUT circuitry. EUTs with mechanical
outputs shall be suitably loaded. When variable electrical or mechanical loading is present in
the actual installation, testing shall be performed under expected worst case conditions. When
active electrical loading (such as a test set) is used, precautions shall be taken to insure the
active load meets the ambient requirements of 4.3.4 when connected to the setup, and that the

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active load does not respond to susceptibility signals. Antenna ports on the EUT shall be
terminated with shielded, matched loads.
Discussion: The application of signals to exercise the electrical interface is necessary to
effectively evaluate performance. Most electronic subsystems on platforms are highly integrated
with large amounts of digital and analog data being transferred between equipment. The use of
actual platform equipment for the interfacing eliminates concerns regarding proper simulation of
the interface. The interfaces must function properly in the presence of induced levels from
susceptibility signals. Required isolation may be obtained by filtering the interface leads at the
active load and either shielding the load or placing it outside of the shielded enclosure. The
filtering should be selected to minimize the influence on the interface electrical properties
specified above. For proper simulation, filtering at the loads should be outside the necessary
bandwidth of the interface circuitry.
Antenna ports are terminated in loads for general setup conditions. Specific test procedures
address electromagnetic characteristics of antenna ports and required modifications to the test
setup.
A.4.3.9 (4.3.9) Operation of EUT.
During emission measurements, the EUT shall be placed in an operating mode which produces
maximum emissions. During susceptibility testing, the EUT shall be placed in its most
susceptible operating mode. For EUTs with several available modes (including software
controlled operational modes), a sufficient number of modes shall be tested for emissions and
susceptibility such that all circuitry is evaluated. The rationale for modes selected shall be
included in the EMITP.
Discussion: The particular modes selected may vary for different test procedures.
Considerations for maximum emissions include conditions which cause the EUT to draw
maximum prime power current, result in greatest activity in interface circuit operation, and
generate the largest current drain on internal digital clock signals. Settings for a radar could be
adjusted such that an output waveform results which has the highest available average power.
Data bus interfaces could be queried frequently to cause constant bus traffic flow. Any modes of
the EUT that are considered mission critical in the installation should be evaluated during
susceptibility testing.
A primary consideration for maximum susceptibility is placing the EUT in its most sensitive
state for reception of intentional signals (maximum gain). An imaging sensor would normally be
evaluated with a scene meeting the most stringent specifications for the sensor. RF receivers are
normally evaluated using an input signal at the minimum signal to noise specification of the
receiver. An additional consideration is ensuring that all electrical interfaces that intentionally
receive data are exercised frequently to monitor for potential responses.
A.4.3.9.1 (4.3.9.1) Operating frequencies for tunable RF equipment.
Measurements shall be performed with the EUT tuned to not less than three frequencies within
each tuning band, tuning unit, or range of fixed channels, consisting of one mid-band frequency
and a frequency within ±5 percent from each end of each band or range of channels.
Discussion: Tuned circuits and frequency synthesis circuitry inside RF equipment typically vary
in characteristics such as response, rejection, and spectral content of emissions as they are set to

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different frequencies. Several test frequencies are required simply to obtain a sampling of the
performance of the EUT across its operating range.
RF equipment that operates in several frequency bands or performs multiple functions is
becoming more common. One example is a radio transceiver with VHF-FM, VHF-AM, and
UHF-AM capability. Other devices are adaptive over large frequency ranges and can be
programmed to perform different functions as the need arises. To meet the intent of the
requirement to perform measurements at three frequencies within each tuning band, tuning unit,
or range of fixed channels, each of the three functions of the radio in the example should be
treated as separate bands, even if they are adjacent in frequency. Similarly, each function of
adaptive RF equipment needs to be separately assessed.
The “value added” of performing all required tests at three frequencies within each band needs to
be weighed against the added cost and schedule. The specific equipment design and intended
function needs to be evaluated for each case.
For example, performing CS101 on a VHF-FM, VHF-AM, and UHF-AM combined receiver–
transmitter would require that the test be performed a minimum of 18 times (3 frequencies * 3
bands * 2 modes). Since CS101 performance generally is related to the power supply design
and load rather than the specific tuned frequency, doing the test for more than a few conditions
may not add much value. If there is a problem, a typical result is “hum” on the secondary power
outputs that is transmitted with the RF or that appears on the output audio of the receiver portion
of the equipment. An appropriate approach for this particular requirement might be to test at one
mid-band frequency for each of the three functions for both transmit and receive (6 tests – 3
frequencies * 2 modes).
Other requirements need to be evaluated similarly. Since CE102 emissions are mainly caused by
power supply characteristics, testing at a mid-band frequency for each band just in the transmit
mode might be adequate. For requirements with frequency coverage that extends into the
operating frequency range of the equipment, such as RE102, CE106, and RS103, testing at three
frequencies per band may be necessary.
A.4.3.9.2 (4.3.9.2) Operating frequencies for spread spectrum equipment.
Operating frequency requirements for two major types of spread spectrum equipment shall be as
follows:
a. Frequency hopping. Measurements shall be performed with the EUT utilizing a hop set
which contains a minimum of 30% of the total possible frequencies. This hop set shall
be divided equally into three segments at the low, mid, and high end of the EUTs
operational frequency range.
b. Direct sequence. Measurements shall be performed with the EUT processing data at
the highest possible data transfer rate.
Discussion: During testing it is necessary to operate equipment at levels that they will
experience during normal field operations to allow for a realistic representation of the emission
profile of the EUT during radiated and conducted testing and to provide realistic loading and
simulation of the EUT during radiated and conducted susceptibility testing.

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Frequency hopping: Utilization of a hopset that is distributed across the entire operational
spectrum of the EUT will help assure that internal circuitry dependent on the exact EUT transmit
frequency being used is active intermittently during processing of the entire pseudo random
stream. The fast operating times of hopping receivers/transmitters versus the allowable
measurement times of the measurement receivers being used (4.3.10.3) will allow a
representative EUT emission signature to be captured.
Direct sequence: Requiring the utilization of the highest data transfer rate used in actual
operation of the EUT should provide a representative worst-case radiated and conducted
emission profile. Internal circuitry will operate at its highest processing rate when integrating
the data entering the transmitter, and then resolving (disintegrating) the data back once again on
the receiver end. Additionally, the data rate will need to be an area of concentration during all
susceptibility testing.
A.4.3.9.3 (4.3.9.3) Susceptibility monitoring.
The EUT shall be monitored during susceptibility testing for indications of degradation or
malfunction. This monitoring is normally accomplished through the use of built-in-test (BIT),
visual displays, aural outputs, and other measurements of signal outputs and interfaces.
Monitoring of EUT performance through installation of special circuitry in the EUT is
permissible; however, these modifications shall not influence test results.
Discussion: Most EUTs can be adequately monitored through normal visual and aural outputs,
self diagnostics, and electrical interfaces. The addition of special circuitry for monitoring can
present questions related to its influence on the validity of the test results and may serve as an
entry or exit point for electromagnetic energy.
The monitoring procedure needs to be specified in the EMITP and needs to include allowances
for possible weaknesses in the monitoring process to assure the highest probability of finding
regions of susceptibility.
A.4.3.10 (4.3.10) Use of measurement equipment.
Measurement equipment shall be as specified in the individual test procedures of this standard.
Any frequency selective measurement receiver may be used for performing the testing described
in this standard provided that the receiver characteristics (that is, sensitivity, selection of
bandwidths, detector functions, dynamic range, and frequency of operation) meet the constraints
specified in this standard and are sufficient to demonstrate compliance with the applicable
limits. Typical instrumentation characteristics may be found in ANSI C63.2.
Discussion: Questions frequently arise concerning the acceptability for use of measurement
receivers other than instruments that are specifically designated "field intensity meters" or "EMI
receivers." Most questions are directed toward the use of spectrum analyzers. These
instruments are generally acceptable for use. However, depending on the type, they can present
difficulties that are not usually encountered with the other receivers. Sensitivity may not be
adequate in some frequency bands requiring that a low noise preamplifier be inserted before the
analyzer input. Impulse type signals from the EUT with broad spectral content may overload the
basic receiver or preamplifier. The precautions of 4.3.7.3 must be observed. Both of these
concerns can usually be adequately addressed by the use of a preselector with the analyzer.
These devices typically consist of a tunable filter which tracks the analyzer followed by a
preamplifier.

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ANSI C63.2 represents a coordinated position from industry on required characteristics of

instrumentation receivers. This document can be consulted when assessing the performance of a
particular receiver.
Many of the test procedures require non-specialized instrumentation that is used for many other
purposes. The test facility is responsible for selecting instrumentation that has characteristics
capable of satisfying the requirements of a particular test procedure.
Current probes used for EMI testing are more specialized instrumentation. These devices are
current transformers with the circuit under test forming a single turn primary. They are designed
to be terminated in 50 ohms. Current probes are calibrated using transfer impedance that is the
ratio of the voltage output of the probe across 50 ohms to the current through the probe. Probes
with higher transfer impedance provide better sensitivity. However, these probes also result in
more series impedance added to the circuit with a greater potential to affect the electrical current
level. The series impedance added by the probe is the transfer impedance divided by the number
of turns in the secondary winding on the probe. Typical transfer impedances are 5 ohms or less.
Typical added series impedance is 1 ohm or less.
A.4.3.10.1 (4.3.10.1) Detector.
A peak detector shall be used for all frequency domain emission and susceptibility
measurements. This device detects the peak value of the modulation envelope in the receiver
bandpass. Measurement receivers are calibrated in terms of an equivalent Root Mean Square
(RMS) value of a sine wave that produces the same peak value. When other measurement devices
such as oscilloscopes, non-selective voltmeters, or broadband field strength sensors are used for
susceptibility testing, correction factors shall be applied for test signals to adjust the reading to
equivalent RMS values under the peak of the modulation envelope.
Discussion: The function of the peak detector and the meaning of the output indication on the
measurement receiver are often confusing. Although there may appear to be an inherent
discrepancy in the use of the terms "peak" and "RMS" together, there is no contradiction. All
detector functions (that is peak, carrier, field intensity, and quasi-peak) process the envelope of
the signal present in the receiver intermediate frequency (IF) section. All outputs are calibrated
in terms of an equivalent RMS value. For a sine wave input to the receiver, the signal envelope
in the IF section is a DC level and all detectors produce the same indicated RMS output.
Calibration in terms of RMS is necessary for consistency. Signal sources are calibrated in terms
of RMS. If a 0 dBm (107 dBμV) unmodulated signal is applied to the receiver, the receiver must
indicate 0 dBm (107 dBμV).
If there is modulation present on the signal applied to the receiver, the detectors respond
differently. The IF section of the receiver sees the portion of the applied signal within the
bandwidth limits of the IF. The peak detector senses the largest level of the signal envelope in
the IF and displays an output equal to the RMS value of a sine wave with the same peak. The
specification of a peak detector ensures that the worst case condition for emission data is
obtained. A carrier detector averages the modulation envelope based on selected charge and
discharge time constants.

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Figure A-4 shows the peak detector output for several modulation waveforms. An item of
interest is that for a square wave modulated signal, which can be considered a pulse type
modulation, the receiver can be considered to be displaying the RMS value of the pulse when it
is on. Pulsed signals are often specified in terms of peak power. The RMS value of a signal is
derived from the concept of power, and a receiver using a peak detector correctly displays the
peak power.

IF SIGNAL EQUIVALENT SINE WAVE, SAME PEAK

A A

B B

C C

A B C
RECEIVER OUTPUT INDICATION WILL BE , , , RESPECTIVELY
2 2 2

FIGURE A-4. Peak detector response.

All frequency domain measurements are standardized with respect to the response that a
measurement receiver using a peak detector would provide. Therefore, when instrumentation is
used which does not use peak detection, correction factors must be applied for certain signals.
For an oscilloscope, the maximum amplitude of the modulated sine wave measured from the DC
level is divided by 1.414 (square root of 2) to determine the RMS value at the peak of the
modulation envelope.
Correction factors for other devices are determined by evaluating the response of the
instrumentation to signals with the same peak level with and without modulation. For example,
a correction factor for a broadband field sensor can be determined as follows. Place the sensor in
an unmodulated field and note the reading. Apply the required modulation to the field ensuring
that the peak value of the field is the same as the unmodulated field. For pulse type modulation,

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most signal sources will output the same peak value when modulation is applied. Amplitude
modulation increases the peak amplitude of the signal and caution must be observed. Note the
new reading. The correction factor is simply the reading with the unmodulated field divided by
the reading with the modulated field. If the meter read 10 V/m without modulation and 5 V/m
with modulation, the correction factor is 2. The evaluation should be tried at several frequencies
and levels to ensure that a consistent value is obtained. When subsequently using the sensor for
measurements with the evaluated modulation, the indicated reading is multiplied by the
correction factor to obtain the correct reading for peak detection.
A.4.3.10.2 (4.3.10.2) Computer-controlled instrumentation.
A description of the operations being directed by software for computer-controlled
instrumentation shall be included in the EMITP. Verification techniques used to demonstrate
proper performance of the software shall also be included. If commercial software is being used
then, as a minimum, the manufacturer, model and revision of the software needs to be provided.
If the software is developed in-house, then documentation needs to be included that describes the
methodology being used for the control of the test instrumentation and how the software
revisions are handled.
Discussion: Computer software obviously provides excellent opportunities for automating
testing. However, it also can lead to errors in testing if not properly used or if incorrect code is
present. It is essential that users of the software understand the functions it is executing, know
how to modify parameters (such as transducer or sweep variables) as necessary, and perform
sanity checks to ensure that the overall system performs as expected. As a minimum, the
following data should be included in the EMITP: sweep times, how correction factors are
handled, how final data are determined and presented, and an audit trail that provides details on
what part of the software controls which functions.
A.4.3.10.3 (4.3.10.3) Emission testing.

A.4.3.10.3.1 (4.3.10.3.1) Bandwidths.

The measurement receiver bandwidths listed in Table II shall be used for emission testing. These
bandwidths are specified at the 6 dB down points for the overall selectivity curve of the
receivers. Video filtering shall not be used to bandwidth limit the receiver response. If a
controlled video bandwidth is available on the measurement receiver, it shall be set to its
greatest value. Larger receiver bandwidths may be used; however, they may result in higher
measured emission levels. NO BANDWIDTH CORRECTION FACTORS SHALL BE APPLIED
TO TEST DATA DUE TO THE USE OF LARGER BANDWIDTHS.

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TABLE II. Bandwidth and measurement time.

Frequency Range 6 dB Dwell Time* Minimum Measurement Time

Bandwidth Analog Measurement Receiver*
30 Hz - 1 kHz 10 Hz 0.15 sec 0.015 sec/Hz
1 kHz - 10 kHz 100 Hz 0.015 sec 0.15 sec/kHz
10 kHz - 150 kHz 1 kHz 0.015 sec 0.015 sec/kHz
150 kHz - 30 MHz 10 kHz 0.015 sec 1.5 sec/MHz
30 MHz - 1 GHz 100 kHz 0.015 sec 0.15 sec/MHz
Above 1 GHz 1 MHz 0.015 sec 15 sec/GHz
* Alternative scanning technique. Multiple faster sweeps with the use of a maximum hold
function may be used if the total scanning time is equal to or greater than the Minimum
Measurement Time defined above.

Discussion: The bandwidths specified in Table II are consistent with the recommended
available bandwidths and the bandwidth specification technique for receivers contained in ANSI
C63.2. Existing receivers have bandwidths specified in a number of different ways. Some are
given in terms of 3 dB down points. The 6 dB bandwidths are usually about 40% greater than
the 3 dB values. Impulse bandwidths are usually very similar to the 6 dB bandwidths. For
Gaussian shaped bandpasses, the actual value is 6.8 dB.
The frequency break point between using a 1 kHz and 10 kHz bandwidth was modified from 250
kHz to 150 kHz in this version of the standard to harmonize with commercial EMI standards.
In order not to restrict the use of presently available receivers that do not have the specified
bandwidths, larger bandwidths are permitted. The use of larger bandwidths can produce higher
detected levels for wide bandwidth signals. The prohibition against the use of correction factors
is included to avoid any attempts to classify signals. A previous version of this standard
eliminated the concept of classification of emissions as broadband or narrowband in favor of
fixed bandwidths and single limits. Emission classification was a controversial area often poorly
understood and handled inconsistently among different facilities.
The sensitivity of a particular receiver is an important factor in its suitability for use in making
measurements for a particular requirement. RE102 is usually the most demanding requirement.
The sensitivity of a receiver at room temperature can be calculated as follows:
Sensitivity in dBm = -114 dBm/MHz + bandwidth (dBMHz) + noise figure (dB)
As noted in the equation, reducing the noise figure is the only way (cryogenic cooling is not
practical) to improve sensitivity for a specified bandwidth. The noise figure of receivers can
vary substantially depending on the front end design. System noise figure can be improved
through the use of low noise preamplifiers. The resulting noise figure of a preamplifier/receiver

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combination can be calculated from the following. All numbers are real numbers. Conversion to
decibels (10 log) is necessary to determine the resulting sensitivity in the above formula:
System noise figure = preamp noise figure + (receiver noise figure)/(preamp gain)
Since preamplifiers are broadband devices, issues of potential overload need to be addressed.
Separate preselectors, which are available for some spectrum analyzers, usually combine a
tracking filter with a low noise preamplifier to eliminate overload. Preselection is an integral
part of many receivers.
Example of multiple scan times derived from Table II are shown below. The frequency bands
listed do not imply that those entire bands should be scanned at one time. The requirements for
frequency resolution defined in 4.3.10.3.4 “Emission data presentation” must be met.
C1 C2 C3 C4 C5 C6 C7 C8 C9

Start Stop Span Resolution # of steps Dwell Table II Single # of fast

Freq Freq (Hz) Bandwidth time single fast sweeps
(Hz) (Hz) (Hz) per sweep sweep to equal
step time time one
(sec) (sec) (sec) Table II
sweep

From From C2 – C1 From Table 2*(C3/C4) From C5 * C6 C5/C4 C7/C8

Table II Table II II Table II

30 1000 970 10 194 0.15 29.1 19.4 1.5

1k 10 k 9k 100 180 0.015 2.7 1.8 1.5

10 k 150 k 140 k 1k 280 0.015 4.2 0.28 15

0.15 M 30 M 29.85 M 10 k 5970 0.015 89.55 0.597 150

30 M 1000 M 970 M 100 k 19400 0.015 291 0.194 1500

1G 18 G 17 G 1M 34000 0.015 510 0.034 15000

The multiple scan option can be an effective method for capturing signals that are intermittent
with a low duty cycle rate “On” time and significant “Off” time. Scan times and number of
scans should be controlled for known signal characteristics to enhance the probability of
capturing these signals. Scan times and sweep speeds are subject to limitations per column 8 of
the above table which provides for enough dwell time for the IF filter to respond. Modern
spectrum analyzers/ receivers have inhibits to prevent an uncalibrated sweep resulting from
sweep speeds that are too fast for the final IF filter to respond. These types of signals form a
Binomial type probability distribution for chance of capturing. Given the signal characteristics
and the scanning parameters, the probability of capturing a signal can be reasonably estimated.
Measurement receivers need to operate in a maximum hold mode such that the highest levels
across the frequency band are recorded over the sequence of scans. The signal characteristics
(cycle times) should be included in the EMITR, if available.

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A.4.3.10.3.2 (4.3.10.3.2) Emission identification.

All emissions regardless of characteristics shall be measured with the measurement receiver
bandwidths specified in Table II and compared against the applicable limits. Identification of
emissions with regard to narrowband or broadband categorization is not applicable.
Discussion: Requirements for specific bandwidths and the use of single limits are intended to
resolve a number of problems. Versions of MIL-STD-461 and MIL-STD-462 prior to the “D”
revision had no controls on required bandwidths and provided both narrowband and broadband
limits over much of the frequency range for most emission requirements. The significance of the
particular bandwidths chosen for use by a test facility was addressed by classification of the
appearance of the emissions with respect to the chosen bandwidths. Emissions considered to be
broadband had to be normalized to equivalent levels in a 1 MHz bandwidth. The bandwidths
and classification techniques used by various facilities were very inconsistent and resulted in a
lack of standardization. The basic issue of emission classification was often poorly understood
and implemented. Requiring specific bandwidths with a single limit eliminates any need to
classify emissions.
An additional problem is that emission profiles from modern electronics are often quite complex.
Some emission signatures have frequency ranges where the emissions exhibit white noise
characteristics. Normalization to a 1 MHz bandwidth using spectral amplitude assumptions
based on impulse noise characteristics is not technically correct. Requiring specific bandwidths
eliminates normalization and this discrepancy.
A.4.3.10.3.3 (4.3.10.3.3) Frequency scanning.
For emission measurements, the entire frequency range for each applicable test shall be
scanned. Minimum measurement time for analog measurement receivers during emission testing
shall be as specified in Table II. Synthesized measurement receivers shall step in one-half
bandwidth increments or less, and the measurement dwell time shall be as specified in Table II.
For equipment that operates such that potential emissions are produced at only infrequent
intervals, times for frequency scanning shall be increased as necessary to capture any emissions.
Discussion: For each emission test, the entire frequency range as specified for the applicable
requirement must be scanned to ensure that all emissions are measured.
Continuous frequency coverage is required for emission testing. Testing at discrete frequencies
is not acceptable unless otherwise stated in a particular test procedure. The minimum scan times
listed in Table II are based on two considerations. The first consideration is the response time of
a particular bandwidth to an applied signal. This time is 1/(filter bandwidth). The second
consideration is the potential rates (that is modulation, cycling, and processing) at which
electronics operate and the need to detect the worst case emission amplitude. Emission profiles
usually vary with time. Some signals are present only at certain intervals and others vary in
amplitude. For example, signals commonly present in emission profiles are harmonics of
microprocessor clocks. These harmonics are very stable in frequency; however, their amplitude
tends to change as various circuitry is exercised and current distribution changes.
The first entry in the table for analog measurement receivers of 0.015 sec/Hz for a bandwidth of
10 Hz is the only one limited by the response time of the measurement receiver bandpass. The
response time is 1/bandwidth = 1/10 Hz = 0.1 seconds. Therefore, as the receiver tunes, the
receiver bandpass must include any particular frequency for 0.1 seconds implying that the

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minimum scan time = 0.1 seconds/10 Hz = 0.01 seconds/Hz. The value in the table has been
increased to 0.015 seconds/Hz to ensure adequate time. This increase by a multiplication factor
of 1.5 results in the analog receiver having a frequency in its bandpass for 0.15 seconds as it
scans. This value is the dwell time specified in the table for synthesized receivers for 10 Hz
bandwidths. Since synthesized receivers are required to step in one-half bandwidth increments
or less and dwell for 0.15 seconds, test time for synthesized receivers will be greater than analog
receivers.
The measurement times for other table entries are controlled by the requirement that the receiver
bandpass include any specific frequency for a minimum of 15 milliseconds (dwell time in table),
which is associated with a potential rate of variation of approximately 60 Hz. As the receiver
tunes, the receiver bandpass is required to include any particular frequency for the 15
milliseconds. For the fourth entry in the table of 1.5 seconds/MHz for a 10 kHz bandwidth, the
minimum measurement time is 0.015 seconds/0.01 MHz = 1.5 seconds/MHz. A calculation
based on the response time of the receiver would yield a response time of 1/bandwidth = 1/10
kHz = 0.0001 seconds and a minimum measurement time of 0.0001 seconds/0.01 MHz = 0.01
seconds/MHz. The longer measurement time of 1.5 seconds/MHz is specified in the table. If the
specified measurement times are not adequate to capture the maximum amplitude of the EUT
emissions, longer measurement times should be implemented.
Caution must be observed in applying the measurement times. The specified parameters are not
directly available on measurement receiver controls and must be interpreted for each particular
receiver. Also, the specified measurement times may be too fast for some data gathering devices
such as real-time X-Y recording. Measurement receiver peak hold times must be sufficiently
long for the mechanical pen drive on X-Y recorders to reach the detected peak value. In
addition, the scan speed must be sufficiently slow to allow the detector to discharge after the
signal is detuned so that the frequency resolution requirements of 4.3.10.3.4 are satisfied.
For measurement receivers with a “maximum hold” feature that retains maximum detected levels
after multiple scans over a particular frequency range, multiple faster sweeps that produce the
same minimum test times as implied by Table II are acceptable. For the situation noted in the
requirement concerning equipment that produces emissions at only infrequent intervals, using
the multiple scan technique will usually provide a higher probability of capturing intermittent
data than using one slower scan.
A.4.3.10.3.4 (4.3.10.3.4) Emission data presentation.
Amplitude versus frequency profiles of emission data shall be automatically generated and
displayed at the time of test and shall be continuous. The displayed information shall account
for all applicable correction factors (transducers, attenuators, cable loss, and the like) and shall
include the applicable limit. Manually gathered data is not acceptable except for verification of
the validity of the output. Plots of the displayed data shall provide a minimum frequency
resolution of 1% or twice the measurement receiver bandwidth, whichever is less stringent, and
minimum amplitude resolution of 1 dB. The above resolution requirements shall be maintained
in the reported results of the EMITR.
Discussion: Versions of MIL-STD-462 prior to the “D” revision permitted data to be taken at
the three frequencies per octave for the highest amplitude emissions. This approach is no
longer acceptable. Continuous displays of amplitude versus frequency are required. This

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information can be generated in a number of ways. The data can be plotted real-time as the
receiver scans. The data can be stored in computer memory and later dumped to a plotter.
Photographs of video displays are acceptable; however, it is generally more difficult to meet
resolution requirements and to reproduce data in this form for submittal in an EMITR.
Placement of limits can be done in several ways. Data may be displayed with respect to actual
limit dimensions (such as dBμV/m) with transducer, attenuation, and cable loss corrections made
to the data. An alternative is to plot the raw data in dBμv (or dBm) and convert the limit to
equivalent dBμv (or dBm) dimensions using the correction factors. This second technique has
the advantage of displaying the proper use of the correction factors. Since both the emission
level and the required limit are known, a second party can verify proper placement. Since the
actual level of the raw data is not available for the first case, this verification is not possible.
An example of adequate frequency and amplitude resolution is shown in Figure A-5. 1%
frequency resolution means that two sinusoidal signals of the same amplitude separated by 1% of
the tuned frequency are resolved in the output display so that they both can be seen. As shown
in the figure, 1% of the measurement frequency of 5.1 MHz is 0.051 MHz and a second signal at
5.151 MHz (1 dB different in amplitude on the graph) is easily resolved in the display. The "2
times the measurement receiver bandwidth" criteria means that two sinusoidal signals of the
same amplitude separated by twice the measurement receiver bandwidth are resolved. For the
example shown in Figure A-5, the bandwidth is 0.01 MHz and 2 times this value is 0.02 MHz.
Therefore, the 1% criterion is less stringent and is applicable. 1 dB amplitude resolution means
that the amplitude of the displayed signal can be read within 1 dB. As shown in the figure, the
reviewer can determine whether the signal amplitude is 60 dBμV or 61 dBμV.

EMISSION LEVEL (dBμV)

70

60
5.1 MHz
61 dBμV 5.151 MHz
60 dBμV
50

40

30

20

10
4 5 6 7 8
FREQUENCY (MHZ)

FIGURE A-5. Example of data presentation resolution.

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The difference between resolution and accuracy is sometimes confusing. Paragraph 4.3.1 of the
standard requires 3 dB measurement system accuracy for amplitude while 4.3.10.3.4 of the
standard requires 1 dB amplitude resolution. Accuracy is an indication how precisely a value
needs to be known while resolution is an indication of the ability to discriminate between two
values. A useful analogy is reading time from a watch. A watch typically indicates the time
within one second (resolution) but may be 30 seconds different than the absolute correct time
(accuracy).
A.4.3.10.4 (4.3.10.4) Susceptibility testing.

A.4.3.10.4.1 (4.3.10.4.1) Frequency scanning.

For susceptibility measurements, the entire frequency range for each applicable test shall be
scanned. For swept frequency susceptibility testing, frequency scan rates and frequency step
sizes of signal sources shall not exceed the values listed in Table III. The rates and step sizes
are specified in terms of a multiplier of the tuned frequency (fo) of the signal source. Analog
scans refer to signal sources which are continuously tuned. Stepped scans refer to signal
sources which are sequentially tuned to discrete frequencies. Stepped scans shall dwell at each
tuned frequency for the greater of 3 seconds or EUT response time. Scan rates and step sizes
shall be decreased when necessary to permit observation of a response.
TABLE III. Susceptibility scanning.

Analog Scans Stepped Scans

Frequency Range Maximum Scan Rates Maximum Step Size

30 Hz - 1 MHz 0.0333fo/sec 0.05 fo

1 MHz - 30 MHz 0.00667 fo/sec 0.01 fo

30 MHz - 1 GHz 0.00333 fo/sec 0.005 fo

1 GHz - 18 GHz 0.00167 fo/sec 0.0025 fo

Discussion: For any susceptibility test performed in the frequency domain, the entire frequency
range as specified in the applicable requirement must be scanned to ensure that all potentially
susceptible frequencies are evaluated. Care must be taken to ensure that the scanning type,
analog or stepped, is correctly selected. Note that most ‘Sweep Generators’ are actually digital
synthesized generators and the “Stepped” scan rates must be used.
The scan rates and step sizes in Table III are structured to allow for a continuous change in value
with frequency for flexibility. Computerized test systems could be programmed to change
values very frequently. A more likely application is to block off selected bands for scanning and
to base selections of scan rate or step size on the lowest frequency. Computerized test systems
could be programmed to calculate the step size for each step. For example, if 1 - 2 GHz were
selected, the maximum step at 1.5 GHz would be: 0.0025 x 1.5 GHz = 3.75 MHz. Both
automatic and manual scanning are permitted.

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The two primary areas of concern for frequency scanning for susceptibility testing are response
times for EUTs to react to stimuli and how sharply the responses tune with frequency, normally
expressed as quality factor (Q). Both of these items have been considered in the determination
of the scan rates and step sizes in Table III. The table entries are generally based on the
assumption of a maximum EUT response time of three seconds and Q values of 10, 50, 100, 500,
and 1000 (increasing values as frequency increases in Table III). Since EUT responses are more
likely to occur in approximately the 1 to 200 MHz range due to efficient cable coupling based on
wavelength considerations, Q values have been increased somewhat to slow the scan and allow
additional time for observation of EUT responses. More detailed discussions on these items
follow.
The assumption of a maximum response time of three seconds is considered to be appropriate for
a large percentage of possible cases. There are several considerations. While the electronics
processing the interfering signal may respond quickly, the output display may take some time to
react. Outputs that require mechanical motion such as meter movements or servo driven devices
will generally take longer to show degradation effects than electronic displays such as video
screens. Another concern is that some EUTs will only be in particularly susceptible states
periodically. For example, sensors feeding information to a microprocessor are typically
sampled at specific time intervals. It is important that the susceptibility stimuli be located at any
critical frequencies when the sensor is sampled. The time intervals between steps and sweep
rates in Table III may need to be modified for EUTs with unusually long response times.
Some concern has been expressed on the susceptibility scan rates and the impact that they would
have on the length of time required to conduct a susceptibility test. The criteria of Table III
allow the susceptibility scan rate to be adjusted continually as the frequency is increased;
however, as a practical matter, the rate would most likely only be changed once every octave or
decade. As an example, Table A-I splits the frequency spectrum up into ranges corresponding to
Table III and frequency ranges of some of the requirements. Actual test times were measured in
a laboratory allowing for settling time and leveling. The total test time to run RS103 from
2 MHz to 18 GHz for a stepped scan is 168 minutes for one polarization. Similarly, an analog
scan would result in a total test time of approximately 100 minutes. These times are based on
continuously calculating the next frequency using the present tuned frequency and the allowed
step size. It must be emphasized that the scan speeds should be slowed down if the EUT
response time or Q are more critical than those used to establish the values in Table III. Note
that the sweep times in the table should be used as programmed times for a scan. Maximum
allowable step sizes must be used. If scanning techniques employing alternative calculations,
such as using the step size at the beginning frequency of an octave for the entire octave, larger
test times will result.
Q is expressed as fo/BW where fo is the tuned frequency and BW is the width in frequency of the
response at the 3 dB down points. For example, if a response occurred at 1 MHz at a
susceptibility level of 1 V and the same response required 1.414 V (3 dB higher in required
drive) at 0.95 and 1.05 MHz, the Q would be 1 MHz/(1.05 - 0.95 MHz) or 10. Q is primarily
influenced by resonances in filters, interconnecting cabling, physical structure, and cavities. The
assumed Q values are based on observations from various types of testing. The step sizes in
Table III are one half of the 3 dB bandwidths of the assumed value of Q ensuring that test
frequencies will lie within the resonant responses.

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TABLE A-I. Susceptibility testing times.

Maximum Actual
Frequency Range
Step Size Scan Time
(minutes)
30 Hz - 150 kHz 0.05 fo 16
150 kHz – 1 MHz 0.05 fo 4
1 MHz – 2 MHz 0.01 fo 5
2 MHz – 30 MHz 0.01 fo 20
30 MHz – 1 GHz 0.005 fo 54
1 GHz – 18 GHz 0.0025 fo 94
18 GHz – 40 GHz 0.0025 fo 28

Below approximately 200 MHz, the predominant contributors are cable and interface filter
resonances. There is loading associated with these resonances which dampens the responses and
limits most values of Q to less than 50. Above 200 MHz, structural resonances of enclosures and
housings start playing a role and have higher values of Q due to less dampening. Above
approximately 1 GHz, aperture coupling with excitation of cavities will be become dominant.
Values of Q are dependent on frequency and on the amount of material contained in the cavity.
Larger values of Q result when there is less material in the volume. A densely packaged
electronics enclosure will exhibit significantly lower values of Q than an enclosure with a higher
percentage of empty volume. Q is proportional to Volume/(Surface Area X Skin Depth). The
value of Q also tends to increase with frequency as the associated wavelength becomes smaller.
EUT designs with unusual configurations that result in high Q characteristics may require that
the scan rates and step sizes in Table III be decreased for valid testing.
RF processing equipment presents a special case requiring unique treatment. Intentionally tuned
circuits for processing RF can have very high values of Q. For example, a circuit operating at
1 GHz with a bandwidth of 100 kHz has a Q of 1 GHz/100 kHz or 10,000.
Automatic leveling used to stabilize the amplitude of a test signal for stepped scans may require
longer dwell times than one second at discrete frequencies. The signal will take time to settle
and any EUT responses during the leveling process should be ignored.
A.4.3.10.4.2 (4.3.10.4.2) Modulation of susceptibility signals.
Susceptibility test signals for CS114 and RS103 shall be pulse modulated (on/off ratio of 40 dB
minimum) at a 1 kHz rate with a 50% duty cycle.
Discussion: Modulation is usually the effect that degrades EUT performance. The wavelengths
of the RF signal cause efficient coupling to electrical cables and through apertures (at higher
frequencies). Non-linearities in the circuit elements detect the modulation on the carrier. The

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circuits may then respond to the modulation depending upon detected levels, circuit bandpass
characteristics, and processing features.
Pulse modulation at a 1 kHz rate, 50% duty cycle, (alternately termed 1 kHz square wave
modulation) is specified for several reasons. One kHz is within the bandpass of most analog
circuits such as audio or video. The fast rise and fall times of the pulse causes the signal to have
significant harmonic content high in frequency and can be detrimental to digital circuits.
Response of electronics has been associated with energy present and a square wave results in
high average power. The modulation encompasses many signal modulations encountered in
actual use. The square wave is a severe form of amplitude modulation used in communications
and broadcasting. It also is a high duty cycle form of pulse modulation representative of radars.
Care needs to be taken in implementing 1 kHz, 50% duty cycle, pulse modulation (on/off ratio of
40 dB) using some signal sources. Most higher frequency signal sources have either internal
pulse modulation or an external port for pulse modulation. This function switches the output on
and off without affecting the amplitude of the unmodulated signal, provided that the strength of
the modulation signal is adequate. For other signal sources, particularly at lower frequencies, the
external amplitude modulation (AM) port needs to be driven to a minimum of 99 % depth of
modulation (equivalent to 40 dB on/off ratio) to simulate pulse modulation. The output signal
will essentially double in amplitude compared to an unmodulated signal for this type of input.
Depending on the type of testing being performed and the technique of monitoring applied
signals, this effect may or may not influence the results. Use of an AM port can be substantially
more involved than using a pulse modulation port. The amplitude of the input signal directly
influences the depth of modulation. There is a potential of exceeding 100% depth of modulation,
which will result in signal distortion. Since the on/off ratio requirement is stringent, it is
necessary to view the output signal on an oscilloscope to set the appropriate depth of modulation.
Another complication is that the bandwidth of AM ports is usually less than pulse ports. Driving
the port with a pulse shape may result in difficulty in setting the source for a minimum of 99%.
MIL-STD-461A required that the worst case modulation for the EUT be used. Worst case
modulation usually was not known or determined. Also, worst case modulation may not be
related to modulations seen in actual use or may be very specialized. The most typical
modulations used below approximately 400 MHz have been amplitude modulation at either 400
or 1000 Hz (30 to 80%) or pulse modulation, 50% duty cycle, at 400 or 1000 Hz. These same
modulations have been used above 400 MHz together with pulse modulation at various pulse
widths and pulse repetition frequencies. Continuous wave (CW - no modulation) has also
occasionally been used. CW typically produces a detected DC level in the circuitry and affects
certain types of circuits. In general, experience has shown that modulation is more likely to
cause degradation. CW should be included as an additional requirement when assessing circuits
that respond only to heat such as electroexplosive devices. CW should not normally be used as
the only condition.
Consideration should be given to applying a secondary 1 Hz modulation (where the normal 1
kHz square wave modulated waveform is completely turned on and off every 500 milliseconds)
for certain subsystems with low frequency response characteristics, such as aircraft flight control
subsystems. This modulation simulates characteristics of some transmitters such as HF radios in
single sideband operation (no carrier), where a transmitted voice signal will cause the RF to be
present only when a word is spoken. The dilemma with using this modulation is that the

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potential response of some subsystems may be enhanced, while others may be less responsive.
In the latter case, the 500 millisecond off period allows the subsystem to recover from effects
introduced during the “on” period.
A.4.3.10.4.3 (4.3.10.4.3) Thresholds of susceptibility.
Susceptibilities and anomalies that are not in conformance with contractual requirements are
not acceptable. However, all susceptibilities and anomalies observed during conduct of the test
need to be documented. When susceptibility indications are noted in EUT operation, a threshold
level shall be determined where the susceptible condition is no longer present. Thresholds of
susceptibility shall be determined as follows and described in the EMITR:
a. When a susceptibility condition is detected, reduce the interference signal until the EUT
recovers.
b. Reduce the interference signal by an additional 6 dB.
c. Gradually increase the interference signal until the susceptibility condition reoccurs.
The resulting level is the threshold of susceptibility.
d. Record this level, frequency range of occurrence, frequency and level of greatest
susceptibility, and other test parameters, as applicable.
Discussion: It is usually necessary to test at levels above the limits to ensure that the test signal
is at least at the required level. Determination of a threshold of susceptibility is necessary when
degradations or anomalies are present to assess whether requirements are met. This information
should be included in the EMITR. Threshold levels below limits are unacceptable.
The specified steps to determine thresholds of susceptibility standardize a particular technique.
An alternative procedure sometimes utilized in the past was to use the value of the applied signal
where the EUT recovers (step a above) as the threshold. Hysteresis type effects are often present
where different values are obtained for the two procedures.
Distortion of sinusoidal susceptibility signals caused by non-linear effects in power amplifiers
can lead to erroneous interpretation of results. When distortion is present, the EUT may actually
respond to a harmonic of the intended susceptibility frequency, where the required limit may be
lower. When frequency selective receivers are used to monitor the injected level, distortion itself
does not prevent a valid susceptibility signal level from being verified at the intended frequency.
However, harmonic levels should be checked when susceptibility is present to determine if they
are influencing the results. When broadband sensors are being used such as in portions of
RS103, distortion can result in the sensor incorrectly displaying the required signal level at the
intended frequency. In this case, distortion needs to be controlled such that correct levels are
measured.
A.4.3.11 (4.3.11) Calibration of measuring equipment.
Test equipment and accessories required for measurement in accordance with this standard
shall be calibrated in accordance with ANSI/NCSL Z540-1 or ISO 10012 or under an approved
calibration program traceable to the National Institute for Standards and Technology. In
particular, measurement antennas, current probes, field sensors, and other devices used in the
measurement loop shall be calibrated at least every 2 years unless otherwise specified by the
procuring activity, or when damage is apparent.

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Discussion: Calibration is typically required for any measurement device whose characteristics
are not verified through use of another calibrated item during testing. For example, it is not
possible during testing to determine whether an antenna used to measure radiated emissions is
exhibiting correct gain characteristics. Therefore, these antennas require periodic calibration.
Conversely, a power amplifier used during radiated susceptibility testing often will not require
calibration since application of the proper signal level is verified through the use of a separate
calibrated field sensing device. Other amplifier applications such as the use of a signal pre-
amplifier in front of a measurement receiver would require calibration of the amplifier
characteristics since the specific gain versus frequency response is critical and is not separately
verified.
A.4.3.11.1 (4.3.11.1) Measurement system test.
At the start of each emission test, the complete test system (including measurement receivers,
cables, attenuators, couplers, and so forth) shall be verified by injecting a known signal, as
stated in the individual test procedure, while monitoring system output for the proper indication.
When the emission test involves an uninterrupted set of repeated measurements (such as
evaluating different operating modes of the EUT) using the same measurement equipment, the
measurement system test needs to be accomplished only one time.
Discussion: The end-to-end system check prior to emission testing is valuable in demonstrating
that the overall measurement system is working properly. It evaluates many factors including
proper implementation of transducer factors and cable attenuation, general condition and setting
of the measurement receiver, damaged RF cables or attenuators, and proper operation of
software. Details on implementation are included in the individual test procedures.
A.4.3.11.2 (4.3.11.2) Antenna factors.
Factors for test antennas shall be determined in accordance with SAE ARP-958.
Discussion: SAE ARP-958 provides a standard basis for determining antenna factors emission
testing. A caution needs to be observed in trying to apply these factors in applications other than
EMI testing. The two antenna technique for antennas such as the biconical and double ridge
horns is based on far field assumptions which are not met over much of the frequency range.
Although the factors produce standardized results, the true value of the electric field is not
necessarily being provided through the use of the factor. Different measuring sensors need to be
used when the true electric field must be known.

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A.5. DETAILED REQUIREMENTS

A.5.1 (5.1) General.

This section specifies detailed emissions and susceptibility requirements and the associated test
procedures. Table IV is a list of the specific requirements established by this standard identified
by requirement number and title. General test procedures are included in this section. Specific
test procedures are implemented by the Government approved EMITP. All results of tests
performed to demonstrate compliance with the requirements are to be documented in the EMITR
and forwarded to the Command or agency concerned for evaluation prior to acceptance of the
equipment or subsystem. Design procedures and techniques for the control of EMI shall be
described in the EMICP. Approval of design procedures and techniques described in the
EMICP does not relieve the supplier of the responsibility of meeting the contractual emission,
susceptibility, and design requirements.
TABLE IV. Emission and susceptibility requirements.

Requirement Description
CE101 Conducted Emissions, Power Leads, 30 Hz to 10 kHz
CE102 Conducted Emissions, Power Leads, 10 kHz to 10 MHz
CE106 Conducted Emissions, Antenna Terminal, 10 kHz to 40 GHz
CS101 Conducted Susceptibility, Power Leads, 30 Hz to 150 kHz
CS103 Conducted Susceptibility, Antenna Port, Intermodulation, 15 kHz to
10 GHz
CS104 Conducted Susceptibility, Antenna Port, Rejection of Undesired
Signals, 30 Hz to 20 GHz
CS105 Conducted Susceptibility, Antenna Port, Cross-Modulation, 30 Hz to
20 GHz
CS106 Conducted Susceptibility, Transients, Power Leads
CS109 Conducted Susceptibility, Structure Current, 60 Hz to 100 kHz
CS114 Conducted Susceptibility, Bulk Cable Injection, 10 kHz to 200 MHz
CS115 Conducted Susceptibility, Bulk Cable Injection, Impulse Excitation
CS116 Conducted Susceptibility, Damped Sinusoidal Transients, Cables and
Power Leads, 10 kHz to 100 MHz
RE101 Radiated Emissions, Magnetic Field, 30 Hz to 100 kHz
RE102 Radiated Emissions, Electric Field, 10 kHz to 18 GHz
RE103 Radiated Emissions, Antenna Spurious and Harmonic Outputs, 10 kHz
to 40 GHz

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TABLE IV. Emission and susceptibility requirements – Continued.

Requirement Description
RS101 Radiated Susceptibility, Magnetic Field, 30 Hz to 100 kHz
RS103 Radiated Susceptibility, Electric Field, 2 MHz to 40 GHz
RS105 Radiated Susceptibility, Transient Electromagnetic Field

Discussion: The applicability of individual requirements in Table IV for a particular equipment

or subsystem is dependent upon the platforms where the item will be used. The electromagnetic
environments present on a platform together with potential degradation modes of electronic
equipment items play a major role regarding which requirements are critical to an application.
For example, emissions requirements are tied to protecting antenna-connected receivers on
platforms. The operating frequency ranges and sensitivities of the particular receivers on-board
a platform, therefore, influence the need for certain requirements.
The EMICP, EMITP, and EMITR are important elements in documenting design efforts for
meeting the requirements of this standard, testing approaches which interpret the generalized test
procedures in this standard, and reporting of the results of testing. The EMICP is a mechanism
instituted to help ensure that contractors analyze equipment design for EMI implications and
include necessary measures in the design for compliance with requirements. Approval of the
document does not indicate that the procuring activity agrees that all the necessary effort is
stated in the document. It is simply a recognition that the design effort is addressing the correct
issues.
The susceptibility limits are the upper bound on the range of values for which compliance is
required. The EUT must also provide required performance at any stress level below the limit.
For example, if the limit for radiated susceptibility to electric fields is 10 V/m, the EUT must
also meet its performance requirements at 5 V/m or any other field less than or equal to 10 V/m.
There have been cases documented where equipment (such as equipment with automatic gain
control circuitry) was not susceptible to radiated electric fields at given frequencies at the limit
level but was susceptible to the environment at the same frequencies when exposed to fields
below the limit level.
In the “B” and “C’ versions of MIL-STD-461, separate requirements were included to deal
specifically with mobile electric power units as UM04 equipment. The intent of the present
version of MIL-STD-461 is that the requirements for this type of equipment are platform
dependent and should simply be the same as any other equipment associated with that platform
as listed in Table IV.

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A.5.1.1 (5.1.1) Units of frequency domain measurements.

All frequency domain limits are expressed in terms of equivalent Root Mean Square (RMS) value
of a sine wave as would be indicated by the output of a measurement receiver using peak
envelope detection (see 4.3.10.1).
Discussion: A detailed discussion is provided on peak envelope detection in 4.3.10.1. A
summary of output of the detector for several input waveforms is as follows. For an
unmodulated sine wave, the output simply corresponds to the RMS value of the sine wave. For a
modulated sine wave, the output is the RMS value of an unmodulated sine wave with the same
absolute peak value. For a signal with a bandwidth greater than the bandwidth of the
measurement receiver, the output is the RMS value of an unmodulated sine wave with the same
absolute peak value as the waveform developed in the receiver bandpass.
A.5.2 (5.2) EMI control requirements versus intended installations.
Table V summarizes the requirements for equipment and subsystems intended to be installed in,
on, or launched from various military platforms or installations. When an equipment or
subsystem is to be installed in more than one type of platform or installation, it shall comply with
the most stringent of the applicable requirements and limits. An "A" entry in the table means the
requirement is applicable. An "L" entry means the applicability of the requirement is limited as
specified in the appropriate requirement paragraphs of this standard; the limits are contained
herein. An "S" entry means the procuring activity must specify the applicability and limit
requirements in the procurement specification. Absence of an entry means the requirement is
not applicable.

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TABLE V. Requirement matrix.

Equipment and Subsystems Installed Requirement Applicability

In, On, or Launched From the
Following Platforms or Installations

CE101
CE102
CE106
CS101
CS103
CS104
CS105
CS106
CS109
CS114
CS115
CS116
RE101
RE102
RE103
RS101
RS103
RS105
Surface Ships A A L A S S S A L A S A A A L A A L
Submarines A A L A S S S A L A S L A A L L A L
Aircraft, Army, Including Flight Line A A L A S S S A A A A A L A A L
Aircraft, Navy L A L A S S S A A A L A L L A L
Aircraft, Air Force A L A S S S A A A A L A
Space Systems, Including Launch A L A S S S A A A A L A
Vehicles
Ground, Army A L A S S S A A A A L L A
Ground, Navy A L A S S S A A A A L A A L
Ground, Air Force A L A S S S A A A A L A

Discussion: Discussion on each requirement as it relates to different platforms is contained in

the sections on the individual requirements.
A.5.3 (5.3) Emission and susceptibility requirements, limits, and test procedures.
Individual emission or susceptibility requirements and their associated limits and test
procedures are grouped together in the following sections. The applicable frequency range and
limit of many emission and susceptibility requirements varies depending on the particular
platform or installation. The test procedures included in this section are valid for the entire
frequency range specified in the procedure; however, testing only needs to be performed over
the frequency range specified for the particular platform or installation.
Discussion: In this version of MIL-STD-461, the test procedures for individual requirements
follow directly after the applicability and limit statements. The discussion for the individual
requirements is separated into these two areas.
A.5.4 (5.4) CE101, conducted emissions, power leads, 30 Hz to 10 kHz.
Applicability and limits: The requirements are applicable to leads that obtain power from
sources that are not part of the EUT. There is no requirement on output leads from power
sources. Since power quality standards are normally used to govern the characteristics of output
power, there is no need for separate EMI requirements on output leads.

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The limits are in terms of current because of the difficulty in controlling the power source
impedance in test facilities at lower frequencies. This type of control would be necessary to
specify the limits in terms of voltage. Emission current levels will be somewhat independent of
power source impedance variations as long as the impedance of the emission source is large
relative to the power source impedance.
For surface ships and submarines, the intent of this requirement is to control the effects of
conducted emissions peculiar to the shipboard power distribution system. Harmonic line
currents are limited for each electrical load connected to the power distribution system. Power
quality for surface ships and submarines is controlled by MIL-STD-1399-300A.
The surface ships and submarine power distribution systems (ship's primary power) supplied by
the ship’s alternators is 440 V, 60 Hz, 3-phase, 3-wire, ungrounded. Although ship's primary
power is ungrounded, there exists a virtual alternating current (AC) ground at each electrical
load due to capacitance to chassis. The unbalance between the virtual grounds at each electrical
load causes AC currents to flow in the hull of the submarine. These hull currents can degrade
the performance of electronic equipment, upset ground detectors, and counteract degaussing.
Hull currents are controlled by limiting the amplitude of harmonic currents conducted on the
power distribution system wiring for each electrical load. The limit is based on maintaining total
harmonic voltage distortion of the ship power distribution system within 5% of the supply
voltage with the contribution from any single harmonic being less than 3%. In addition to the
hull current concern, total harmonic distortion of the supply voltage waveform greater than 5% is
above the tolerance of most electronic equipment, induction motors, magnetic devices, and
measuring devices.
For Army aircraft, the primary concern is to ensure that the EUT does not corrupt the power
quality (allowable voltage distortion) on the power buses present on the platform. The Army
aircraft limits are based on relating the allowable current flowing into a 1.0 ohm impedance to
MIL-STD-704 requirements on voltage distortion. The Army limit includes approximately a
20 dB margin with respect to MIL-STD-704 to allow for contributions from multiple emission
sources.
For Navy aircraft, the requirement is applicable for installations using anti-submarine warfare
(ASW) equipment. The primary mission of ASW aircraft is to detect and locate submarines.
Unacceptable levels of emission currents in the frequency range of this test would limit the
detection and processing capabilities of the Magnetic Anomaly Detection (MAD) and Acoustic
Sensor systems. The MAD systems must be able to isolate a magnetic disturbance in the earth's
magnetic field of less than one part in 50,000. In present aircraft, the full sensitivity of the MAD
systems is not available due to interference produced by onboard equipment. Low frequency
interference effects in the 30 Hz to 10 kHz can be a problem for Acoustic Sensor systems.
Possible tailoring of the requirements by the procuring activity is to impose the requirement if
sensitive receivers operating in the frequency range of the requirement are to be installed on a
platform or to modify the limit based on the particular characteristics of the power system
onboard the platform.
Another possible tailoring of the requirement by the procuring activity is for cases where high
current loads exist (filter size may be massive to meet limit), where power distribution wiring

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has short lengths, or where dedicated returns run with the high sides (versus structure return).
For these cases, the use of a 5 μH LISN may be appropriate, but it must be approved by the
procuring activity. If a 5 μH LISN is used, the following modifications to the CE101
requirement could be applicable. Figure A-6 shows limits that will preserve MIL-STD-704
power quality and minimize filter size, regardless of EUT current load. The low frequency
plateau of each curve is shown for a 1 Amp load at the power frequency. The low frequency
plateau shifts upward for higher currents by adding a factor of 20*log (load current in Amperes).
The limit extends to 150 kHz instead of 10 kHz. The limit at 150 kHz is fixed and calculated to
coincide with the CE102 limit at 150 kHz, based on the impedance of a 5 μH LISN. Thus the
slope of the limit curve between the scaled 2 kHz point and the fixed 150 kHz is a function of
load current. For an AC load, the scan should start just below 400 cycles so that the 400 cycle
load current can be used to properly scale the limit, even though the AC limit does not begin
until the second harmonic.
Below 2 kHz, limit scales as 20*log (steady-state current, Amps rms)
120
Curve #1
110
Curve #2
100
Curve #3
90
dBuA

80
NOMINAL EUT SOURCE VOLTAGE APPLICABLE
70 CURVE
66 dBuA, fixed
115 Vac, 400 Hz #1
60 28 Vdc #2
270 Vdc #3 56 dBuA, fixed
50
0.01 0.1 1 10 100
150 kHz
Frequency kHz

FIGURE A-6. CE101 limits for a 5 μH LISN.

Test procedures: Emission levels are determined by measuring the current present on each
power lead. The LISNs will have little influence on the results of this testing. The circuit
characteristics of the LISN will help stabilize measurements near 10 kHz; however, the LISN
parameters will not be significant over most of the frequency range of the test.
Current is measured because of the low impedances present over most of the frequency range of
the test. Current levels will be somewhat independent of power source impedance variations as
long as the impedance of the emission source is significant in relation to the power source
impedance. However, at frequencies where the shielded room filters in the test facility resonate
(generally between 1 and 10 kHz), influences on measured currents can be expected.

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During the measurement system check, the signal generator may need to be supplemented with a
power amplifier to obtain the necessary current 6 dB below the applicable limit.
The value of the resistor “R” in Figure CE101-5 is not specified because a particular value is not
critical. Whatever value is convenient for measurement and possible matching of the signal
generator can be used.
A possible alternative measurement tool in this frequency range is a wave analyzer using a Fast
Fourier Transform algorithm. Use of this type of instrumentation requires specific approval by
the procuring activity.
An alternative test procedure for high current loads from 30 Hz – 150 kHz may be desirable.
While the CE101 test method can be used without modification with these load current-
dependent limits, it is desirable, especially for 400 Hz loads, to eliminate the LISN altogether,
since it is not relevant to the measurement. A 5 μH LISN as described in the DISCUSSION of
4.3.6 may be used; however, it will influence the measurement somewhat. Another contributor
to high power source impedance is the EMI test facility electrical filters, which typically
resonate below 10 kHz and can have impedance as high as 50 ohms at a resonance. For AC
loads, which are drawing harmonic currents below 10 kHz, it may be desirable to short out the
EMI filters. For DC power, this effect is easily accomplished by placing a large capacitor across
the power source. For AC power this approach is not practical. For AC power, the input and
output ends of the facility filter would have to be shorted together to bypass the series
inductance. If the line-to-ground capacitance of the filter then causes power factor problems, it
may be necessary to bypass the filters altogether and bring power into the test chamber from an
unfiltered source. The technical criterion for low source impedance is that the power waveform
as loaded by the EUT has suitably low distortion. The distortion as measured when the EUT is
energized is:
Allowable distortion (%) = (MIL-STD-704 total distortion (%)) x (EUT load current/power
source rated load current)
For an AC bus, use of a distortion meter is desirable rather than a measurement receiver. If a
distortion meter is not available, then the peak AC voltage should be measured open circuit and
as loaded by the EUT, the difference between these divided by the open-circuit peak potential is
subject to the limit above.
A.5.5 (5.5) CE102, conducted emissions, power leads, 10 kHz to 10 MHz.
Applicability and limits: The requirements are applicable to leads that obtain power from
sources that are not part of the EUT. There is no requirement on output leads from power
sources.
The basic concept in the lower frequency portion of the requirement is to ensure that the EUT
does not corrupt the power quality (allowable voltage distortion) on the power buses present on
the platform. Examples of power quality documents are MIL-STD-704 for aircraft, MIL-STD-
1399 for ships, MIL-STD-1539 for space systems, and MIL-STD-1275 for military vehicles.
Since power quality standards govern allowable distortion on output power, there is no need for
separate EMI requirements on output leads. The output power leads are treated no differently
than any other electrical interface. This standard does not directly control the spectral content of

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signals present on electrical interfaces. Waveform definitions and distortion limits are specified
in documents such as interface control documents. In the case of output power, the quality of the
power must be specified over an appropriate frequency range so that the user of the power can
properly design for its characteristics. This situation is true whether the power source is a
primary source such as 115 V, 400 Hz, or a ± 15 VDC low current supply. A significant indirect
control on spectral content exists in the RE102 limits which essentially require that appropriate
waveform control and signal transmission techniques be used to prevent unacceptable radiation
(see discussion on CE102 limit placement and RE102 relationship below).
Since voltage distortion is the basis for establishing power quality requirements, the CE102 limit
is in terms of voltage. The use of standardized line impedance over the frequency range of this
test provides for the convenient measurement of the voltage as developed across this impedance.
In previous versions of MIL-STD-461, a current measurement into a 10 μF feedthrough
capacitor was specified. The intent of the capacitor was to provide an RF short of the power lead
to the ground plane. It was difficult to interpret the significance of the current limit with respect
to platform applications. The presence of standardized impedance is considered to reflect more
closely the electrical characteristics of the power buses in platforms.
Of the power quality documents reviewed, MIL-STD-704 is the only one with a curve specifying
an amplitude versus frequency relationship for the allowable distortion. The CE102 limits
require that amplitude decays with increasing frequency similar to the requirements of MIL-
STD-704. Common requirements are specified for all applications since the concerns are the
same for all platforms.
The basic limit curve for 28 V is placed approximately 20 dB below the power quality curve in
MIL-STD-704. There are several reasons for the placement. One reason is that a number of
interference sources present in different subsystems and equipments on a platform may be
contributing to the net interference voltage present at a given location on the power bus.
Assuming that the interference sources are not phase coherent, the net voltage will be the square
root of the sum of the squares of the voltages from the individual sources. A second reason is
that the actual impedance in an installation will vary from the control impedance with actual
voltages being somewhat higher or lower than that measured during the test. Therefore, some
conservatism needs to be included in the limit.
The relaxation for other higher voltage power sources is based on the relative levels of the power
quality curves on ripple for different operating voltages.
At higher frequencies, the CE102 limit serves as a separate control from RE102 on potential
radiation from power leads that may couple into sensitive antenna-connected receivers. The
CE102 limits have been placed to ensure that there is no conflict with the RE102 limit.
Emissions at the CE102 limit should not radiate above the RE102 limit. Laboratory experiments
on coupling from a 2.5 meter power lead connected to a line impedance stabilization network
have shown that the electric field detected by the RE102 rod antenna is flat with frequency up to
approximately 10 MHz and is approximately equal to (x-40) dBμV/m, where “x” is the voltage
expressed in dBμV. For example, if there is a signal level of 60 dBμV on the lead, the detected
electric field level is approximately 20 dBμV/m.
Tailoring of the requirements in contractual documents may be desirable by the procuring
activity. Adjusting the limit line to more closely emulate a spectral curve for a particular power

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quality standard is one possibility. Contributions from multiple interference sources need to be
considered as noted above. If antenna-connected receivers are not present on the platform at the
higher frequencies, tailoring of the upper frequency of the requirement is another possibility.
The requirement is limited to an upper frequency of 10 MHz due to the allowable 2.5 meter
length of power lead in the test setup approaching resonance. Any conducted measurements
become less meaningful above this frequency. If tailoring is done to impose the requirement at
higher frequencies, the test setup should be modified for CE102 to shorten the allowable length
of the power leads.
If the alternate CE101 limit and procedure for high current loads has been used below 150 kHz,
then CE102 may start at 150 kHz instead of 10 kHz. In this case, a 5 μH LISN (such as the one
described in the DISCUSSION under 4.3.6) should be used. While the CE102 limit does not
change, the use of the 5 μH LISN provides relief in EMI filter design for both differential and
common mode noise. Differential mode noise is a voltage source which will establish the same
voltage in a 5 or 50 μH LISN, but the 5 μH LISN allows more current to flow for the same
potential, so the filter attenuation requirements are lower. Common mode noise is a current
source, and the lower impedance of the 5 μH LISN means that for a given current less measured
voltage results below about 3 MHz. At 3 MHz and above the 5 and 50 μH LISNs have the same
impedance, but it is much easier to filter in this high frequency 50 ohm region than between
10 kHz and 3 MHz.
Test procedures: Emission levels are determined by measuring the voltage present at the output
port on the LISN.
The power source impedance control provided by the LISN is a critical element of this test. This
control is imposed due to wide variances in characteristics of shielded room filters and power
line impedances among various test agencies and to provide repeatability through
standardization. The LISN standardizes this impedance. The impedance present at the EUT
electrical interface is influenced by the circuit characteristics of the power lead wires to the
LISNs. The predominant characteristic is inductance. The impedance starts to deviate
noticeably at approximately 1 MHz where the lead inductance is about 13 ohms.
A correction factor must be included in the data reduction to account for the 20 dB attenuator
and for voltage drops across the coupling capacitor. This capacitor is in series with a parallel
combination of the 50 ohm measurement receiver and the 1 kilohm LISN resistor. The two
parallel resistances are equivalent to 47.6 ohms. The correction factor equals:
20 log10(1 + 5.60x10-9f2)1/2/(7.48x10-5f)
where f is the frequency of interest expressed in Hz. This equation is plotted in Figure A-7. The
correction factor is 4.45 dB at 10 kHz and drops rapidly with frequency.
The upper measurement frequency is limited to 10 MHz because of resonance conditions with
respect to the length of the power leads between the EUT and LISN. As noted in 4.3.8.6.2 of the
main body of the standard, these leads are between 2.0 and 2.5 meters long. Laboratory
experimentation and theory show a quarter-wave resonance close to 25 MHz for a 2.5 meter
lead. In the laboratory experiment, the impedance of the power lead starts to rise significantly at
10 MHz and peaks at several thousand ohms at approximately 25 MHz. Voltage measurements
at the LISN become largely irrelevant above 10 MHz.

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 MIL-STD-461F
APPENDIX A

dB

0
10 100 200
FREQUENCY (kHz)

FIGURE A-7. Correction factor for 50 μH LISN coupling capacitor.

The 0.25 μF coupling capacitor in the LISN allows approximately 3.6 V to be developed across
the 50 ohm termination on the signal port for 115 V, 400 Hz, power sources. The 20 dB
attenuator is specified in the test procedure to protect the measurement receiver and to prevent
overload. Sources of 60 Hz pose less of a concern.
An oscilloscope is necessary for the measurement system check in Figure CE102-1 to ensure that
the actual applied voltage is measured accurately at 10 kHz and 100 kHz and maintains a
sinusoidal shape. The LISN presents a 50 ohm load impedance to a 50 ohm signal generator
only for frequencies of approximately 300 kHz or higher (see Figure 7). Since a 50 ohm signal
generator is essentially an ideal voltage source in series with 50 ohms, the amplitude display
setting of the generator is correct only when it is terminated in a matched impedance of 50 ohms.
Under this condition the voltage splits between the two 50 ohm resistances. If the output is
measured directly with a high impedance instrument, such as an oscilloscope, the indicated
voltage is twice the amplitude setting. The load seen by the signal generator varies with
frequency and the voltage at the LISN will also vary.
An area of concern for this test procedure is the potential to overload the measurement receiver
due to the line voltage at the power frequency. Overload precautions are discussed in paragraph
4.3.7.3 of this standard. When an overload condition is predicted or encountered, a rejection
filter can be used to attenuate the power frequency. A correction factor must be then included in
the emission data to account for the filter loss with respect to frequency.
The CE102 test procedure for a 5 μH LISN is identical to that using a 50 μH LISN. The only
difference is starting the test at 150 kHz. No correction factor is necessary for the coupling
capacitor in the 5 μH LISN above 150 kHz.

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A.5.6 (5.6) CE106, conducted emissions, antenna terminal, 10 kHz to 40 GHz.

Applicability and limits: The requirement is applicable for transmitters, receivers and
amplifiers. The basic concern is to protect antenna-connected receivers both on and off the
platform from being degraded due to radiated interference from the antenna associated with the
EUT. The limit for transmitters in the transmit mode is placed primarily at levels which are
considered to be reasonably obtainable for most types of equipment. Suppression levels that are
required to eliminate all potential electromagnetic compatibility situations are often much more
severe and could result in significant design penalties. The limit for receivers and transmitters in
standby is placed at a level that provides reasonable assurance of compatibility with other
equipment. Common requirements are specified for all applications since the concerns are the
same for all platforms.
As an example of an antenna coupling situation, consider a 10 watt VHF-AM transmitter
operating at 150 MHz and a UHF-AM receiver with a sensitivity of -100 dBm tuned to 300 MHz
with isotropic antennas located 10 meters apart. The requirement is that the transmitter second
harmonic at 300 MHz must be down 50 + 10 log 10 = 60 dB. The free space loss equation.
PR/PT = (λ2GTGR)/(4πR)2 indicates an isolation of 42 dB between the two antennas.
PR = Received Power GR = Receive Antenna Gain = 1
PT = Transmitted Power GT = Transmitter Antenna Gain = 1
λ = Wavelength = 1 meter R = Distance between Antennas = 10 meters
A second harmonic at the limit would be 60 + 42 = 102 dB down at the receiver. 102 dB below
10 Watts (40 dBm) is -62 dBm which is still 38 dB above the receiver sensitivity. The level that
is actually required not to cause any degradation in the receiver is -123 dBm. This value results
because the worst-case situation occurs when the interfering signal is competing with the
sidebands of the intentional signal with a signal amplitude at the receiver sensitivity. For a
standard tone of 30% AM used to verify sensitivity, the sidebands are 13 dB down from the
carrier and a 10 dB signal-to-noise ratio is normally specified. To avoid problems, the
interfering signal must, therefore, be 13 + 10 = 23 dB below -100 dBm or -123 dBm. This
criterion would require the second harmonic to be 121 dB down from the transmitter carrier that
could be a difficult task. Harmonic relationships can sometimes be addressed through frequency
management actions to avoid problems.
Assessing the 34 dBμV (-73 dBm) requirement for standby, the level at the receiver would be
-115 dBm which could cause some minimal degradation in the presence of a marginal intentional
signal.
Greater antenna separation or antenna placement not involving direct line of sight would
improve the situation. Also, the VHF antenna may be poorer than isotropic in the UHF band.
CE106 does not take into account any suppression associated with frequency response
characteristics of antennas; however, the results of the case cited are not unusual. RE103, which
is a radiated emission control on spurious and harmonic outputs, includes assessment of antenna
characteristics.
Since the free space loss equation indicates that isolation is proportional to the wavelength
squared, isolation values improve rapidly as frequency increases. Also, antennas are generally

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 MIL-STD-461F
APPENDIX A

more directional in the GHz region and receivers tend to be less sensitive due to larger
bandwidths.
The procuring activity may consider tailoring contractual documents by establishing suppression
levels based on antenna-to-antenna coupling studies on the particular platform where the
equipment will be used. Another area could be relaxation of requirements for high power
transmitters. The standard suppression levels may result in significant design penalties. For
example, filtering for a 10,000 watt HF transmitter may be excessively heavy and substantially
attenuate the fundamental frequency. Engineering trade-offs may be necessary.
Test procedures: Since the test procedures measure emissions present on a controlled
impedance, shielded, transmission line, the measurement results should be largely independent
of the test setup configuration. Therefore, it is not necessary to maintain the basic test setup
described in the main body of this standard.
The CE106 procedure uses a direct coupled technique and does not consider the effect that the
antenna system characteristics will have on actual radiated levels.
The selection of modulation for transmitters and frequency, input power levels, and modulation
for amplifiers can influence the results. The procedure requires that parameters that produce the
worst case emission spectrum be used. The most complicated modulation will typically produce
the worst case spectrum. The highest allowable drive level for amplifiers usually produces the
worst harmonics and spurious outputs. However, some amplifiers with automatic gain controls
may produce higher distortion with drive signals set to the lowest allowable input due to the
amplifier producing the highest gain levels. The details of the analysis on the selection of test
parameters should be included in the EMITP.
Figure CE106-3 is used for receivers and transmitters in the stand-by mode. The purpose of the
attenuator pad in Figure CE106-3 is to establish a low VSWR for more accurate measurements.
Its nominal value is 10 dB, but it can be smaller, if necessary, to maintain measurement
sensitivity.
The setup in Figure CE106-1 is used for low power transmitters in which the highest
intentionally generated frequency does not exceed 40 GHz. The attenuator pad should be
approximately 20 dB or large enough to reduce the output level of the transmitter sufficiently so
that it does not damage or overload the measurement receiver. The rejection network in the
figure is tuned to the fundamental frequency of the EUT and is intended to reduce the transmitter
power to a level that will not desensitize or induce spurious responses in the measurement
receiver. Both the rejection network and RF pad losses must be adjusted to maintain adequate
measurement system sensitivity. The total power reaching the measurement receiver input
should not exceed the maximum allowable level specified by the manufacturer. All rejection and
filter networks must be calibrated over the frequency range of measurement.
The setup of Figure CE106-2 is for transmitters with high average power. For transmitters with
an integral antenna, it is usually necessary to measure the spurious emissions by the radiated
procedures of RE103.
Some caution needs to be exercised in applying Table II. For spurious and harmonic emissions
of equipment in the transmit mode, it is generally desirable for the measurement receiver
bandwidth to be sufficiently large to include at least 90% of the power of the signal present at a

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 MIL-STD-461F
APPENDIX A

tuned frequency. This condition is required if a comparison is being made to a power

requirement in a specification. Spurious and harmonic outputs generally have the same
modulation characteristics as the fundamental. Since this procedure measures relative levels of
spurious and harmonic signal with respect to the fundamental, it is not necessary for the
measurement receiver to meet the above receiver bandwidth to signal bandwidth criterion.
However, if the measurement receiver bandwidth does not meet the criterion and spurious and
harmonic outputs are located in frequency ranges where this standard specifies a bandwidth
different than that used for the fundamental, the measurement receiver bandwidth should be
changed to that used at the fundamental to obtain a proper measurement.
For EUTs having waveguide transmission lines, the measurement receiver needs to be coupled to
the waveguide by a waveguide to coaxial transition. Since the waveguide acts as a high-pass
filter, measurements are not necessary at frequencies less than 0.8 fco, where fco is the waveguide
cut-off frequency.
A.5.7 (5.7) CS101, conducted susceptibility, power leads, 30 Hz to 150 kHz.
Applicability and limits: The requirement is applicable to power input leads that obtain power
from other sources that are not part of the EUT. There is no requirement on power output leads.
The basic concern is to ensure that equipment performance is not degraded from ripple voltages
associated with allowable distortion of power source voltage waveforms.
The required signal is applicable only to the high sides on the basis that the concern is
developing a differential voltage across the power input leads to the EUT. The series injection
technique in the test procedure results in the voltage dropping across the impedance of the EUT
power input circuitry. The impedance of the power return wiring is normally insignificant with
respect to the power input over most of the required frequency range. Common mode voltages
evaluations are addressed by other susceptibility tests such as CS114 and RS103. Injection on a
power return will result in the same differential voltage across the power input; however, the
unrealistic condition will result in a large voltage at the return connection to the EUT with
respect to the ground plane.
Similar to CE102, the limits are based on a review of the power quality standards with emphasis
toward the spectral content curves present in MIL-STD-704. Rather than having a separate
curve for each possible power source voltage, only two curves are specified. The voltage
amplitude specified is approximately 6 dB above typical power quality limits, although the limit
has been somewhat generalized to avoid complex curves. The margin between the limit and the
power quality standard is necessary to allow for variations in performance between
manufactured items.
The difference between the limits for CE102 and CS101 of approximately 26 dB should not be
viewed as a margin. The CE102 limit is placed so that ripple voltages do not exceed that
allowed by the power quality standards due to interference contributions from multiple EUTs.
Therefore, the power quality standard is the only valid basis of comparison.
The primary tailoring consideration for the procuring activity for contractual documents is
adjustment of the limit to follow more closely a particular power quality standard.

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APPENDIX A

Test procedures: Since the applied voltage is coupled in series using a transformer, Kirchhoff's
voltage law requires that the voltage appearing across the transformer output terminals must drop
around the circuit loop formed by the EUT input and the power source impedance. The voltage
level specified in the limit is measured across the EUT input because part of the transformer
induced voltage can be expected to drop across the source impedance.
Earlier EMI standards introduced a circuit for a phase shift network which was intended to
cancel out AC power waveforms and allow direct measurement of the ripple present across the
EUT. While these devices very effectively cancel the power waveform, they return the incorrect
value of the ripple and are not acceptable for use. The networks use the principle of inverting
the phase of the input power waveform, adding it to the waveform (input power plus ripple)
across the EUT, and presumably producing only the ripple as an output. For a clean power
waveform, the network would perform properly. However, the portion of the ripple that drops
across the power source impedance contaminates the waveform and gets recombined with the
ripple across the EUT resulting in an incorrect value.
Voltages will appear across the primary side of the injection transformer due to the EUT current
load at the power frequency. Larger current loads will result in larger voltages and are the
predominant concern. These voltages can cause potential problems with the power amplifier.
The circuit arrangement in Figure A-8 will substantially reduce this voltage and provide
protection for the amplifier. This effect is accomplished by using a dummy load equal to the
EUT and wiring the additional transformer so that its induced voltage is equal to and 180 degrees
out of phase with the induced voltage in the injection transformer. If possible, the dummy load
should have the same power factor as the EUT.
On initial turn on, DC to DC power switching converters can create large voltages on the
primary side of the injection transformer that can damage the power amplifier. A precaution is
to place a 5 ohm resistor across the primary and to disconnect the transformer during initial turn
on.
The injected signal should be maintained as a sinusoid. Saturation of the power amplifier or
coupling transformer may result in a distorted waveform.
If the return side of power is not connected to the shielded room ground, the oscilloscope may
need to be electrically “floated” using an isolation transformer to correctly measure the injected
voltage resulting in a potential shock hazard. Differential probe amplifiers are available which
will convert a differential measurement between the high side and an isolated ground to a single-
ended measurement where the measurement device can be grounded. These probes have an
output that is suitable for measurement with either an oscilloscope or a high impedance,
frequency selective, receiver (provided the receiver can tolerate the high input voltage).

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 MIL-STD-461F
APPENDIX A

AC POWER
INPUTS ONLY

VOLTAGE
EUT
MONITOR

SIGNAL POWER

GENERATOR AMPLIFIER
DUMMY
LOAD
SAME
CURRENT
AS EUT

IDENTICAL
ISOLATION
TRANSFORMERS

FIGURE A-8. CS101 power amplifier protection.

A.5.8 (5.8) CS103, conducted susceptibility, antenna port, intermodulation, 15 kHz to 10

GHz.
Applicability and limits: The intent of this requirement is to control the response of antenna-
connected receiving subsystems to in-band signals resulting from potential intermodulation
products of two signals outside of the intentional passband of the subsystem produced by non-
linearities in the subsystem. The requirement can be applied to receivers, transceivers,
amplifiers, and the like. Due to the wide diversity of subsystem designs being developed, the
applicability of this type of requirement and appropriate limits need to be determined for each
procurement. Also, requirements need to be specified that are consistent with the signal
processing characteristics of the subsystem and the particular test procedures to be used to verify
the requirement.
One approach for determining levels required for the out-of-band signals is from an analysis of
the electromagnetic environments present and characteristics of receiving antennas. However,
levels calculated by this means will often place unreasonable design penalties on the receiver.
For example, if an external environment of 200 V/m is imposed on a system, an isotropic
antenna at 300 MHz will deliver 39 dBm to the receiver. This level represents a severe design
requirement to many receivers. An alternative approach is to simply specify levels that are
within the state-of-the-art for the particular receiver design.

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 MIL-STD-461F
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This requirement is most applicable to fixed frequency, tunable, superheterodyne receivers.

Previous versions of this standard required normal system performance with the two out-of-band
signals to be 66 dB above the level required to obtain the standard reference output for the
receiver. One signal was raised to 80 dB above the reference in the 2 to 25 MHz and 200 to 400
MHz bands to account for transmissions from HF and UHF communication equipment.
Maximum levels for both signals were limited to 10 dBm. As an example, conventional
communication receivers commonly have sensitivities on the order of -100 dBm. For this case,
the 66 dB above reference signal is at -34 dBm and the 80 dB above reference signal is at -20
dBm. Both are substantially below the 10 dBm maximum used in the past.
For other types of receivers, application of this requirement is often less straightforward and care
must be taken to ensure that any applied requirements are properly specified. Many receivers are
designed to be interference or jam resistant and this feature may make application of this
requirement difficult or inappropriate.
One complicating factor is that one of the out-of-band signals typically is modulated with a
waveform normally used by the receiver. For receivers that process a very specific modulation,
the issue exists whether an out-of-band signal can reasonably be expected to contain that
modulation. Another complicating factor is related to the potential intermodulation products
resulting from two signals. Responses from intermodulation products can be predicted to occur
when fo = mf1 ± nf2 where fo is the operating frequency of the receiver, m and n are integers, and
f1 and f2 are the out-of-band signals. For receivers which continuously change frequency (such
as frequency agile or frequency hopping), the relationship will be true only for a portion of the
operating time of the receiver, unless the out-band-signals are also continuously tuned or the
receiver operating characteristics are modified for the purpose of evaluation.
Test procedures: No test procedures are provided in the main body of this standard for this
requirement. Because of the large variety of receiver designs being developed, the requirements
for the specific operational characteristics of a receiver must be established before meaningful
test procedures can be developed. Only general testing techniques are discussed in this
appendix.
Intermodulation testing can be applied to a variety of receiving subsystems such as receivers, RF
amplifiers, transceivers and transponders.
Several receiver front-end characteristics must be known for proper testing for intermodulation
responses. These characteristics generally should be determined by test. The maximum signal
input that the receiver can tolerate without overload needs to be known to ensure that the test
levels are reasonable and that the test truly is evaluating intermodulation effects. The bandpass
characteristics of the receiver are important for determining frequencies near the receiver
fundamental fo that will be excluded from test. Requirements for this test are generally
expressed in terms of a relative degree of rejection by specifying the difference in level between
potentially interfering signals and the established sensitivity of the receiver under test.
Therefore, determination of the sensitivity of the receiver is a key portion of the test.
The basic concept with this test is to combine two out-of-band signals and apply them to the
antenna port of the receiver while monitoring the receiver for an undesired response. One of the
out-of-band signals is normally modulated with the modulation expected by the receiver. The
second signal is normally continuous wave (CW). Figure A-9 shows a general setup for this test.

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 MIL-STD-461F
APPENDIX A

SIGNAL
SOURCE NO. 1

FILTERS, MEASUREMENT
ATTENUATORS, RECEIVER
AS NEEDED

3 PORT
3 PORT 3 PORT
NETWORK, EUT
NETWORK NETWORK
IF NEEDED

FILTERS, FILTERS,
ATTENUATORS, OUTPUT
ATTENUATORS, MONITOR
AS NEEDED AS NEEDED

SIGNAL SIGNAL
SOURCE NO. 2 SOURCE NO. 3,
IF NEEDED

FIGURE A-9. CS103 General test setup.

For applications where the receiver would not provide an indication of interference without a
receive signal being present, a third signal can be used at the fundamental. This arrangement
may also be suitable for some receivers that process a very specialized type of modulation which
would never be expected on an out-of-band signal. An option is for the two out-of-band signals
to be CW for this application.
The frequency of the two out-of-band signals should be set such that fo = 2f1 - f2 where fo is the
tuned frequency of the receiver and f1 and f2 are the frequencies of the signal sources. This
equation represents a third order intermodulation product, which is the most common response
observed in receivers. f1 and f2 should be swept or stepped over the desired frequency range
while maintaining the relationship in the equation. It is important to verify that any responses
noted during this test are due to intermodulation responses. Responses can result from simply
lack of rejection to one of the applied signals or from harmonics of one of the signal sources.
Turning off each signal source in turn and noting whether the response remains can demonstrate
the source of the response.
For receivers with front-end mixing and filtering in an antenna module, the test may need to be
designed to be performed on a radiated basis. All signals would need to be radiated and
assurances provided that any observed intermodulation products are due to the receiver and not
caused by items in the test area. The EMITP would need to address antenna types, antenna

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 MIL-STD-461F
APPENDIX A

locations, antenna polarizations and field measurement techniques. This test would probably
need to be performed in an anechoic chamber.
For frequency hopping receivers, one possible approach is choose an fo within the hop set and set
up the signals sources as described above. The performance of the receiver could then be
evaluated as the receiver hops. If the frequency hopping receiver has a mode of operation using
just one fixed frequency, this mode should also be tested.
A common error made in performing this test procedure is attributing failures to the EUT which
are actually harmonics of the signal source or intermodulation products generated in the test
setup. Therefore, it is important to verify that the signals appearing at the EUT antenna port are
only the intended signals through the use of a measurement receiver as shown in Figure A-9.
Damaged, corroded, and faulty components can cause signal distortion resulting in misleading
results. Monitoring will also identify path losses caused by filters, attenuators, couplers, and
cables.
Typical data for this test procedure for the EMITR are the sensitivity of the receiver, the levels of
the signal sources, frequency ranges swept, operating frequencies of the receivers, and
frequencies and threshold levels associated with any responses.
A.5.9 (5.9) CS104, conducted susceptibility, antenna port, rejection of undesired signals, 30
Hz to 20 GHz.
Applicability and limits: The intent of this requirement is to control the response of antenna-
connected receiving subsystems to signals outside of the intentional passband of the subsystem.
The requirement can be applied to receivers, transceivers, amplifiers, and the like. Due to the
wide diversity of subsystem designs being developed, the applicability of this type of
requirement and appropriate limits need to be determined for each procurement. Also,
requirements need to be specified that are consistent with the signal processing characteristics of
the subsystem and the particular test procedures to be used to verify the requirement.
One approach for determining levels required for the out-of-band signal can be determined from
an analysis of the electromagnetic environments present and characteristics of receiving
antennas. However, levels calculated by this means will often place unreasonable design
penalties on the receiver. For example, if an external environment of 200 V/m is imposed on a
system, an isotropic antenna at 300 MHz will deliver 39 dBm to the receiver. This level
represents a severe design requirement to many receivers. An alternative approach is to simply
specify levels that are within the state-of-the-art for the particular receiver design.
This requirement is most applicable to fixed frequency, tunable, superheterodyne receivers.
Previous versions of this standard required normal system performance for a 0 dBm signal
outside of the tuning range of the receiver and a signal 80 dB above the level producing the
standard reference output within the tuning range (excluding the receiver passband within the 80
dB points on the selectivity curve). As an example, a conventional UHF communication
receiver operating from 225 MHz to 400 MHz commonly has a sensitivity on the order of -100
dBm. For this case, the 0 dBm level applies below 225 MHz and above 400 MHz. Between 225
MHz and 400 MHz (excluding the passband), the required level is -20 dBm.

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For other types of receivers, application of this requirement is often less straightforward and care
must be taken to ensure that any applied requirements are properly specified. Many receivers are
designed to be interference or jam resistant and this feature may make application of this
requirement difficult or inappropriate.
This requirement is usually specified using either one or two signals. With the one signal
requirement, the signal is out-of-band to the receiver and is modulated with a waveform
normally used by the receiver. No in-band signal is used. For receivers that process a very
specific modulation, the issue exists whether an out-of-band signal can reasonably be expected to
contain that modulation. An alternative is to specify the requirement for two signals. An in-
band signal can be specified which contains the normal receiver modulation. The out-of-band
signal can be modulated or unmodulated with the criterion being that no degradation in reception
of the intentional signal is allowed.
Test procedures: No test procedures are provided in the main body of this standard for this
requirement. Because of the large variety of receiver designs being developed, the requirements
for the specific operational characteristics of a receiver must be established before meaningful
test procedures can be developed. Only general testing techniques are discussed in this
appendix.
Front-end rejection testing can be applied to a variety of receiving subsystems such as receivers,
RF amplifiers, transceivers, and transponders.
Several receiver front-end characteristics must be known for proper testing. These
characteristics generally should be determined by test. The maximum signal input that the
receiver can tolerate without overload needs to be known to ensure that the test levels are
reasonable. The bandpass characteristics of the receiver are important for determining
frequencies near the receiver fundamental that will be excluded from testing. Requirements for
this test are often expressed in terms of a relative degree of rejection by specifying the difference
in level between a potentially interfering signal and the established sensitivity of the receiver
under test. Therefore, determination of the sensitivity of the receiver is a key portion of the test.
The basic concept with this test procedure is to apply out-of-band signals to the antenna port of
the receiver while monitoring the receiver for degradation. Figure A-10 shows a general test
setup for this test. There are two common techniques used for performing this test using either
one or two signal sources. For the one signal source procedure, the signal source is modulated
with the modulation expected by the receiver. It is then swept over the appropriate frequency
ranges while the receiver is monitored for unintended responses. With the two signal source
procedure, a signal appropriately modulated for the receiver is applied at the tuned frequency of
the receiver. The level of this signal is normally specified to be close to the sensitivity of the
receiver. The second signal is unmodulated and is swept over the appropriate frequency ranges
while the receiver is monitored for any change in its response to the intentional signal.

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 MIL-STD-461F
APPENDIX A

FILTERS,
SIGNAL
ATTENUATORS,
SOURCE NO. 1
AS NEEDED

MEASUREMENT
RECEIVER

3 PORT
3 PORT
NETWORK, EUT
NETWORK
IF NEEDED

OUTPUT
MONITOR
SIGNAL FILTERS,
SOURCE NO. 2, ATTENUATORS,
IF NEEDED AS NEEDED

FIGURE A-10. CS104 General test setup.

The two signal source procedure is more appropriate for most receivers. The one signal source
procedure may be more appropriate for receivers that search for a signal to capture since they
may respond differently once a signal has been captured. Some receivers may need to be
evaluated using both procedures to be completely characterized.
For frequency hopping receivers, one possible approach is to use a one signal procedure as if the
EUT did not have a tuned frequency (include frequency scanning across the hop set) to evaluate
the jamming/interference resistance of the receiver. If a frequency hopping receiver has a mode
of operation using just one fixed frequency, this mode should also be tested.
For receivers with front-end mixing and filtering in an antenna module, the test may need to be
designed to be performed on a radiated basis. All signals would need to be radiated and
assurances provided that any observed responses are due to the receiver and not caused by items
in the test area. The EMITP would need to address antenna types, antenna locations, antenna
polarizations, and field measurement techniques. This test would probably need to be performed
in an anechoic chamber.
A common error made in performing this test procedure is attributing failures to the EUT which
are actually harmonics or spurious outputs of the signal source. Therefore, it is important to
verify that the signals appearing at the EUT antenna port are only the intended signals through
the use of a measurement receiver as shown in Figure A-10. Damaged, corroded, and faulty
components can cause signal distortion resulting in misleading results. Monitoring will also
identify path losses caused by filters, attenuators, couplers, and cables.

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Typical data for this test procedure for the EMITR are the sensitivity of the receiver, the levels of
the signal sources, frequency ranges swept, operating frequencies of the receivers, degree of
rejection (dB), and frequencies and threshold levels associated with any responses.
A.5.10 (5.10) CS105, conducted susceptibility, antenna port, cross modulation, 30 Hz to 20
GHz.
Applicability and limits: The intent of this requirement is to control the response of antenna-
connected receiving subsystems to modulation being transferred from an out-of-band signal to an
in-band signal. This effect results from a strong, out-of-band signal near the operating frequency
of the receiver that modulates the gain in the front-end of the receiver and adds amplitude
varying information to the desired signal. The requirement should be considered only for
receivers, transceivers, amplifiers, and the like, which extract information from the amplitude
modulation of a carrier. Due to the wide diversity of subsystem designs being developed, the
applicability of this type of requirement and appropriate limits need to be determined for each
procurement. Also, requirements need to be specified that are consistent with the signal
processing characteristics of the subsystem and the particular test procedure to be used to verify
the requirement.
One approach for determining levels required for the out-of-band signal can be determined from
an analysis of the electromagnetic environments present and characteristics of receiving
antennas. However, levels calculated by this means will often place unreasonable design
penalties on the receiver. For example, if an external environment of 200 V/m is imposed on a
system, an isotropic antenna at 300 MHz will deliver 39 dBm to the receiver. This level
represents a severe design requirement to many receivers. An alternative approach is to simply
specify levels that are within the state-of-the-art for the particular receiver design.
This requirement is most applicable to fixed frequency, tunable, superheterodyne receivers.
Previous versions of this standard required normal system performance with an out-of-band
signal to be 66 dB above the level required to obtain the standard reference output for the
receiver. The maximum level for the signal was limited to 10 dBm. As an example,
conventional communication receivers commonly have sensitivities on the order of -100 dBm.
For this example, the 66 dB above reference signal is at -34 dBm that is substantially below the
10 dBm maximum used in the past.
For other types of receivers, application of this requirement is often less straightforward and care
must be taken to ensure that any applied requirements are properly specified. Many receivers are
designed to be interference or jam resistant and this feature may make application of this
requirement difficult or inappropriate.
One complicating factor is that one of the out-of-band signals typically is modulated with a
waveform normally used by the receiver. For receivers that process a very specific modulation,
the issue exists whether an out-of-band signal can reasonably be expected to contain that
modulation. Another factor is that the out-of-band signal is normally specified to be close to the
receiver operating frequency. For receivers that continuously change frequency (such as
frequency agile or frequency hopping), an appropriate relationship may exist for only short
periods for a fixed frequency out-of-band signal.

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Test procedures: No test procedures are provided in the main body of this standard for this
requirement. Because of the large variety of receiver designs being developed, the requirements
for the specific operational characteristics of a receiver must be established before meaningful
test procedures can be developed. Only general testing techniques are discussed in this
appendix.
Cross modulation testing should be applied only to receiving subsystems such as receivers, RF
amplifiers, transceivers and transponders which extract information from the amplitude
modulation of a carrier.
Several receiver front-end characteristics must be known for proper testing for cross modulation
responses. These characteristics generally should be determined by test. The maximum signal
input that the receiver can tolerate without overload needs to be known to ensure that the test
levels are reasonable. The bandpass characteristics of the receiver are important for determining
frequencies near the receiver fundamental that will be excluded from test. Requirements for this
test are generally expressed in terms of a relative degree of rejection by specifying the difference
in level between potentially interfering signals and the established sensitivity of the receiver
under test. Therefore, determination of the sensitivity of the receiver is a key portion of the test.
The basic concept with this test is to apply a modulated signal out-of-band to the receiver and to
determine whether the modulation is transferred to an unmodulated signal at the receiver's tuned
frequency resulting in an undesired response. There may be cases where the in-band signal
needs to be modulated if the receiver characteristics so dictate. The level of the in-band signal is
normally adjusted to be close to the receiver's sensitivity. The out-of-band signal is modulated
with the modulation expected by the receiver. It is then swept over the appropriate frequency
ranges while the receiver is monitored for unintended responses. Testing has typically been
performed over a frequency range ± the receiver intermediate frequency (IF) centered on the
receiver's tuned frequency. Figure A-8 shows a general setup for this test.
For receivers with front-end mixing and filtering in an antenna module, the test may need to be
designed to be performed on a radiated basis. All signals would need to be radiated and
assurances provided that any responses are due to the receiver and not caused by items in the test
area. The EMITP would need to address antenna types, antenna locations, antenna polarizations
and field measurement techniques. This test would probably need to be performed in an
anechoic chamber.
For frequency hopping receivers, one possible approach is choose an fo within the hop set and set
up the signals sources as described above. The performance of the receiver could then be
evaluated as the receiver hops. If the frequency hopping receiver has a mode of operation using
just one fixed frequency, this mode should also be tested.
It is important to verify that the signals appearing at the EUT antenna port are only the intended
signals through the use of a measurement receiver as shown in Figure A-11. Damaged,
corroded, and faulty components can cause signal distortion resulting in misleading results.
Monitoring will also identify path losses caused by filters, attenuators, couplers, and cables.

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FILTERS,
SIGNAL ATTENUATORS,
SOURCE NO. 1 AS NEEDED

MEASUREMENT
RECEIVER

3 PORT 3 PORT
NETWORK, EUT
NETWORK
IF NEEDED

OUTPUT
MONITOR
FILTERS,
SIGNAL ATTENUATORS,
SOURCE NO. 2 AS NEEDED

FIGURE A-11. CS105 General test setup.

Typical data for this test procedure for the EMITR are the sensitivity of the receiver, the levels of
the signal sources, frequency ranges swept, operating frequencies of the receivers, and
frequencies and threshold levels associated with any responses.
A.5.11 (5.11) CS106, conducted susceptibility, transients, power leads.
Applicability and limits: The requirement is applicable to power input leads on surface ships
and submarines that obtain power from the platform’s primary power source that are not part of
the EUT. There is no requirement on power output leads. The primary concern is to ensure that
equipment performance is not degraded from voltage transients experienced on shipboard power
systems coupling to interface wiring inside enclosures.
Electrical transients occur on all electrical distribution systems and can cause problems in
circuitry which tend to be sensitive to voltage transients, such as latching circuits expecting a
single trigger signal. On submarines and surface ships, these transients can be caused by
switching of inductive loads, circuit breaker (or relay) bounce, and load feedback onto the power
distribution system.
The 400 volt peak, 5 microsecond pulse defined in Figure CS106-1 is a suitable representation of
the typical transient observed on Navy platforms. Measurements of transients on Navy
platforms have shown the transient durations (widths) are predominantly in the 1 – 10
microsecond range. The large majority (> 90%) of the transients measured on both the 115 volt
and 440 volt ac power distribution systems were between 50 and 500 volts peak.

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The Navy submarine community has found the obsolete CS06 of MIL-STD-461 (through
revision C) requirement to be an effective method to minimize risk of transient-related
equipment and subsystem susceptibility. The CS106 type transient test has been successful in
early identification of transient related EMI problems in naval equipment and subsystems. The
Navy has found good correlation between transient related shipboard EMI problems (including
longevity, degraded performance and premature failures) and CS106 susceptibilities. Navy
surface ships are using the CS106 requirement for commonality in the ship community.
The requirement to synchronize the transient to phase positions of the AC waveform which was
present in the heritage CS06 method is not included in the new CS106 requirement. No
technical rationale was ever established historically to perform this action and there are good
arguments against synchronization. Transients generally do not occur at zero crossings and
applied transient suppression techniques have actually taken advantage of this fact by switching
power at a zero crossing. Also, there is no significance to a particular phase position. In
addition, the argument provided for re-establishing a CS106 type transient was based on
crosstalk issues which have no relationship to phase position. This portion of the requirement
could be tailored back in for a particular case if desired by a procuring activity.
Test procedures: Since the applied transient is coupled in series, Kirchhoff’s voltage law states
that the voltage appearing across the transient generator output terminals must drop around the
circuit loop formed by the EUT input and the power source impedance. The transient voltage
level specified in the limit is measured across the EUT input because part of the induced voltage
can be expected to drop across the source impedance. A 10 μF capacitor is added across the
power source to reduce the voltage drop across the power source impedance.
Calibration of the transient generator is performed utilizing a 5 ohm, non-inductive resistor. The
CS106 requirement is met by either the transient signal level, as measured across the EUT power
input, being reached on the power lead or the transient generator calibration set point being
obtained, whichever occurs first.
Figure CS106-1 is a nominal representation of the spike as measured across the 5 ohm, non-
inductive resistor. Characteristics of the waveform can vary by make and model of the generator
employed; particularly the sag or undershoot. The shape of the sag or undershoot is not critical
provided the maximum sag voltage and duration are not exceeded.
If the return side of power is not connected to the shielded room ground, the oscilloscope may
need to be electrically “floated” using an isolation transformer to correctly measure the injected
voltage resulting in a potential shock hazard. Differential probe amplifiers for oscilloscopes are
available which will convert a differential measurement between the high side and an isolated
ground to a single-ended measurement where the measurement device can be grounded. In lieu
of an AC powered oscilloscope “floated” using an isolation transformer, a battery powered
oscilloscope can be used. The battery powered oscilloscope will eliminate the electrical shorting
possibility while using a “floating” oscilloscope.
The 400 V requirement calibrated across a 5 ohm resistive load produces 80 A in the resistor.
When applied to an EUT with a low source impedance, currents greater than 280 A are available
from the specified transient generator with a source impedance ≤ 2.0 Ω. Energy levels can be
substantial.

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A.5.12 (5.12) CS109, conducted susceptibility, structure current, 60 Hz to 100 kHz.

Applicability and limits: This requirement is specialized and is intended to be applied only for
very sensitive equipment (1 μV or better) such as tuned receivers operating over the frequency
range of the test. The basic concern of the requirement is to ensure that equipment does not
respond to magnetic fields caused by currents flowing in platform structure and through EUT
housing materials. The magnetic fields are sufficiently low that there is no concern with most
circuitry.
An estimate can be made of induced voltages that may result from the required CS109 currents.
Magnetic fields act by inducing voltages into loop areas in accordance with Faraday's law
(V = -dφ/dt). For a constant magnetic field perpendicular to a given loop area, Faraday's law
reduces to V = -2πfBA where
f = Frequency of Interest B = Magnetic Flux Density A = Loop Area
Since Faraday's law indicates that these voltages are proportional to frequency, the maximum
voltage from the CS109 currents will result at the 20 kHz knee of the curve for a given loop area.
A drop of 20 dB/decade would result in a constant voltage. Since the curve is dropping at only
10 dB/decade below 20 kHz, the induced voltage will rise as frequency increases. The sharp
drop off above 20 kHz results in decreasing voltages with increasing frequency.
If the 103 dBμA current at 20 kHz specified in the requirement is assumed to spread uniformly
over a cross-sectional dimension of 10 cm, the surface current density and the resulting magnetic
field intensity at the surface would be 1.41 amperes/meter. In air, this value corresponds to
magnetic flux density of 1.77x10-6 Tesla. If it is further assumed that this magnetic field is
uniform over a circuit loop area of 0.001 m2 (such as 20 cm by 0.5 cm) within the enclosure,
Faraday's Law predicts an induced voltage of 222 μV.
Similar calculations at 400 Hz and 100 kHz yield values of 31 μV and 8 μV, respectively.
It is apparent that design considerations such as proper grounding techniques, minimizing of
loop areas, and common mode rejection concepts need to be implemented to prevent potential
problems with very sensitive circuits used in submarines such as low frequency tuned receivers.
However, these levels are well below the sensitivity of typical circuits used in other equipment.
The limit is derived from operational problems due to current conducted on equipment cabinets
and laboratory measurements of response characteristics of selected receivers.
No tailoring is recommended.
Test procedures: Electrical connection needs to be made to the external structure of the EUT
and damage to the external finish should be minimized. Screws or protuberances at ground
potential near the diagonal corners of the EUT should normally be used as test points.
Connections should be made with clip or clamp type leads. If convenient test points are not
available at the diagonal corners, a sharply pointed test probe should be used to penetrate the
finish in place of the clip or clamp type lead.
The requirement to maintain the leads perpendicular to the surface for at least 50 cm is to
minimize effects on the path of current flow along the surface from the magnetic fields caused by
the current in the leads.

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Coupling transformers used to perform CS101 testing are normally suitable for this test. The
electrical isolation provided by the coupling transformer eliminates the need to electrically
“float” the amplifier and signal source that could result in a potential shock hazard.
A.5.13 (5.13) CS114, conducted susceptibility, bulk cable injection, 10 kHz to 400 MHz.
Applicability and limits: The requirements are applicable to all electrical cables interfacing
with the EUT enclosures. The basic concept is to simulate currents that will be developed on
platform cabling from electromagnetic fields generated by antenna transmissions both on and off
the platform. Investigation into aircraft carrier hangar deck electromagnetic environment test
data from 9 aircraft carriers showed that significant HF electric field levels are present.
Measurements from on-board HF transmitters showed field levels in the 2 to 30 MHz band up to
42 V/m in the hanger deck. Therefore, for equipment located in the aircraft hanger deck, the
same limit that is used for non-metallic ships (below decks), is being used in the 2 to 30 MHz
frequency range. In addition, a low frequency limit (77 dBμA) has been added from 4 kHz to 1
MHz for EUTs on surface ships and submarines with solid state power generation (in contrast to
electromechanical generation equipment) to simulate common mode currents that have been
found to be present on AC power cables. The measured common mode currents have exceeded
the previous CS114 Ships (metallic, below decks) and Submarines (internal) limits by up to 50
dB.
An advantage of this type of requirement is that it provides data that can be directly related to
induced current levels measured during platform-level evaluations. An increasingly popular
technique is to illuminate the platform with a low level, relatively uniform field while
monitoring induced levels on cables. Then, either laboratory data can be reviewed or current
injection done at the platform with the measured currents scaled to the full threat level. This
same philosophy has been applied to lightning and electromagnetic pulse testing.
Due to size constraints and available field patterns during radiated susceptibility testing (such as
RS103), it has long been recognized that cabling cannot be properly excited to simulate platform
effects at lower frequencies. The most notable example of this situation is experience with HF
(2 - 30 MHz) radio transmissions. HF fields have caused numerous problems in platforms
through cable coupling. However, equipment items rarely exhibit problems in this frequency
range during laboratory testing.
The limits are primarily derived from testing on aircraft that were not designed to have
intentionally shielded volumes. The basic structure is electrically conductive; however, there
was no attempt to ensure continuous electrical bonding between structure members or to close all
apertures. The shape of the limit reflects the physics of the coupling with regard to resonant
conditions, and the cable length with respect to the interfering frequency wavelength. At
frequencies below resonance, coupling is proportional to frequency (20 dB/decade slope).
Above resonance, coupled levels are cyclic with frequency with a flat maximum value. The 10
dB/decade decrease in the limit level at the upper frequency portion is based on actual induced
levels in the aircraft testing data base when worst-case measurements for the various aircraft are
plotted together. From coupling theory for a specific cable, the decrease would be expected to
be cyclic with frequency with an envelope slope of 40 dB/decade.

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The basic relationship for the limit level in the resonance (flat) portion of the curve is 1.5 mA per
V/m that is derived from worst-case measurements on aircraft. For example, 110 dBμA
corresponds to 200 V/m. At resonance, the effective shielding effectiveness of the aircraft can
be zero. Application of these results to other platforms is reasonable.
The frequency range of 10 kHz to 200 MHz is now standardized for all applications. The
optional frequency range of 200 MHz to 400 MHz is deleted because of the questionable validity
of performing bulk cable measurements at higher frequencies.
For submarines, the CS114 limit now distinguishes between equipment located internal versus
external to the pressure hull. For equipment installed internal to the pressure hull, the curve 2
limit is now specified above 30 MHz to account for portable transmitters used within the
submarine. For equipment located external to the pressure hull, stricter limits are imposed to
more closely reflect the electromagnetic environment. The external CS114 limits should be
applied only to equipment that is required to be fully operational when located above the
waterline. Separate limits are specified, which are less severe, for equipment that is “external” to
the pressure hull but located within the submarine superstructure (metallic boundary).
The limit may be tailored by the procuring activity in contractual documents with a curve whose
amplitude is based on the expected field intensity for the installation and with a breakpoint for
the curve based on the lowest resonance associated with the platform. Tailoring of the frequency
of application can be done based on the operating frequencies of antenna-radiating equipment.
Tailoring should also include transmitters that are not part of the platform. For equipment used
in benign environments, the requirement may not be necessary.
Test procedures: This type of test is often considered as a bulk current test since current is the
parameter measured. However, it is important to note that the test signal is inductively coupled
and that Faraday's law predicts an induced voltage in a circuit loop with the resultant current
flow and voltage distribution dependent on the various impedances present.
The calibration fixture with terminations is a 50 ohm transmission line. Since the injection probe
is around the center conductor within the fixture, a signal is being induced in the loop formed by
the center conductor, the two 50 ohm loads, and the structure of the fixture to which the 50 ohm
loads are terminated. From a loop circuit standpoint, the two 50 ohm loads are in series,
providing a total loop impedance of 100 ohms. Because of the transmission line configuration,
inductance effects are minimized. Measurement of induced current levels is performed by
measuring a corresponding voltage across one of the 50 ohm loads. Since the 50 ohm loads are
in series for the induced signal, the total drive voltage is actually two times that being measured.
The actual current that appears on a tested cable from the pre-calibrated drive signal depends on
the loop impedance associated with the cable and the source impedance characteristics of the
drive probe and amplifier. If the loop impedance is low, such as would often result with an
overall shielded cable, currents greater than those in the calibration fixture will result. The
maximum required current is limited to 6 dB above the pre-calibration level.
In the past, MIL-STD-462 included a test procedure, CS02, which specified capacitive coupling
of a voltage onto individual power leads. As is the case for this test procedure, CS02 assessed
the effect of voltages induced from electromagnetic fields. CS114 improves on CS02 by
inducing levels on all wires at a connector interface simultaneously (common mode) which

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better simulates actual platform use. Also, a deficiency existed with CS02 since the RF signals
were induced only on power leads. This test procedure is applicable to all EUT cabling.
The requirement to generate loop circuit characterization data has been removed from this
version of the standard. The information was not being used as it was originally envisioned.
A commonly used calibration fixture is shown in Figure A-12. Other designs are available. The
top is removable to permit the lower frequency probes to physically fit. The calibration fixture
can be scaled to accommodate larger injection probes. Figure A-13 displays the maximum
VSWR that this calibration fixture should exhibit when measured without a current probe
installed in the fixture. The presence of a probe will usually improve the VSWR of the fixture.

NOTE: VERTICAL CROSS-SECTION AT CENTER OF FIXTURE SHOWN

TOP SHALL BE REMOVEABLE

12.7 mm ALUMINUM
120 mm WIDE

35 mm DIA TYPE N
CONNECTORS (2)
*
120 mm
12.7 mm ALUMINUM
15 mm DIA 180 mm WIDE
BRASS
60 mm PLASTIC COATED
70 mm

230 mm
260 mm

* DIMENSIONS OF OPENING CRITICAL

FIGURE A-12. Typical CS114 calibration fixture.

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3.5

3
VSWR:1

2.5

1.5

0 100 200 300 400

Frequency (MHz)

FIGURE A-13. Maximum VSWR of calibration fixture.

An advantage of this type of conducted testing as compared to radiated susceptibility testing is
that voltage and current levels can be more easily induced on the interfaces that are comparable
to those present in installations. The physical dimensions of the EUT cabling in a test setup are
often not large enough compared to the installation for efficient coupling at lower frequencies.
In the past, some platform-level problems on Navy aircraft could not be duplicated in the
laboratory using the standard test procedures in earlier versions of this standard. It was
determined that differences between the aircraft installation and laboratory setups regarding the
laboratory ground plane and avionics (aircraft electronics) mounting and electrical bonding
practices were responsible. Most avionics are mounted in racks and on mounting brackets. At
RF, the impedances to general aircraft structure for the various mounting schemes can be
significantly different than they are with the avionics mounted on a laboratory ground plane. In
the laboratory, it is not always possible to produce a reasonable simulation of the installation. A
ground plane interference (GPI) test was developed to detect potential failures due to the higher
impedance. In the GPI test, each enclosure of the EUT, in turn, is electrically isolated above the
ground plane and a voltage is applied between the enclosure and the ground plane to simulate
potential differences that may exist in the installation. Since CS114 provides similar common
mode stresses at electrical interfaces as the GPI, the GPI is not included in this standard.
However, the Navy may prefer to perform an additional susceptibility scan for aircraft
applications with an inductor placed between the EUT enclosure and ground plane to more
closely emulate the results of a GPI setup. The primary side of a typical CS101 injection
transformer is considered to be an appropriate inductor.
CS114 has several advantages over the GPI as a general evaluation procedure. The GPI often
results in significant current flow with little voltage developed at lower frequencies. CS114 is a
controlled current test. A concern with the GPI test, which is not associated with CS114, is that

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the performance of interface filtering can be altered due to isolation of the enclosure from the
ground plane. The results of CS114 are more useful since the controlled current can be
compared with current levels present in the actual installation induced from fields. This
technique has commonly been used in the past for certification of aircraft as safe to fly.
Testing is required on both entire power cables and power cables with the returns removed to
evaluate common mode coupling to configurations that may be present in different installations.
In some installations, the power returns are routed with the high side wiring. In other
installations, power returns are tied to system structure near the utilization equipment with
system structure being used as the power return path.
Insertion loss characteristics of injection probes are specified in Figure CS114-2 of the test
procedure. A control on insertion loss has been found to be necessary to obtain consistency in
test results. Insertion loss is measured as shown in Figure A-14. It is the difference in dB of the
power applied to the probe installed in the calibration fixture and the power level detected by the
measurement receiver. Lower insertion loss indicates more efficient coupling. Since the signal
level that is induced in the calibration fixture is equally divided between the 50 ohm coaxial load
and the measurement receiver, the lowest possible loss is 3 dB. The use of a network analyzer or
measurement receiver that includes a tracking generator can simplify the measurement.

Coaxial Load

Injection
Probe

Signal
Generator

Calibration
Fixture
Measurement
Receiver

FIGURE A-14. Insertion loss measurement.

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Techniques using network analyzers or spectrum analyzers with tracking generators can simplify
the measurements for both 5.13.3.4b calibration and 5.13.3.4c EUT testing portions of the
procedure. For example, the output signal can first be set to a predetermined value such as one
mW and the flatness of the signal with frequency can be separately verified through a direct
connection to the receiver. With this same signal then applied to the directional coupler, the
induced level in the calibration fixture can be directly plotted.
The lower frequency limit for ships and submarines has been extended to 4 kHz to simulate
common mode currents that have been found to be present on AC power cables for EUTs
installed on platforms with solid state power generation (ships and submarines). The calibration
limit from 4 kHz to 10 kHz is 77 dBμA. This limit is achievable with 100 watt power amplifier
and an injection probe which complies with the insertion loss requirement of Figure CS114-2.
A possible alternative to the injection probe method below 10 kHz is to utilize a CS101 injection
transformer in each power lead and to drive all in parallel. The common mode current is
measured between the injection transformers and the EUT power input. The alternative method
for a three-phase ungrounded power system is shown schematically in Figure A-15.

Signal
Generator

Measurement
Receiver
Amplifier

Monitor Probe

LISNs
A
EUT B
C
Power
Inputs
Power Leads

FIGURE A-15. CS114 alternate test setup, three phase ungrounded power system.

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A.5.14 (5.14) CS115, conducted susceptibility, bulk cable injection, impulse excitation.
Applicability and limits: The requirements are applicable to all electrical cables interfacing
with EUT enclosures. The basic concern is to protect equipment from fast rise and fall time
transients that may be present due to platform switching operations and external transient
environments such as lightning and electromagnetic pulse. The requirement is intended to
replace "chattering relay" type requirements (RS06 in MIL-STD-461C) commonly used in
procurements of equipment for aircraft applications in the past. The chattering relay has been
criticized as unscientific and non-repeatable. The CS115 requirement has a defined waveform
and a repeatable coupling mechanism.
The 2 nanosecond rise time is consistent with rise times possible for the waveforms created by
inductive devices interrupted by switching actions. The 30 nanosecond pulse width standardizes
the energy in individual pulses. In addition, it separates the rising and falling portions of the
pulse so that each may act independently. Also, each portion may affect different circuits. The 5
ampere amplitude (500 V across 100 ohm loop impedance calibration fixture) covers most
induced levels that have been observed during system-level testing of aircraft to transient
environments. The 30 Hz pulse rate is specified to ensure that a sufficient number of pulses are
applied to provide confidence that the equipment will not be upset.
Many circuit interfaces are configured such that potential upset is possible for only a small
percentage of the total equipment operating time. For example, a microprocessor may
sequentially poll various ports for input information. A particular port may continuously update
information between polling intervals. If the transient occurs at the time the port is accessed, an
upset condition may result. At other times, no effect may occur.
Possible tailoring by the procuring activity for contractual documents is lowering or raising the
required amplitude based on the expected transient environments in the platform. Another
option is to adjust the pulse width based on a particular environment onboard a platform or for
control of the energy content of the pulse.
Test procedures: The excitation waveform from the generator is a trapezoidal pulse. The
actual waveform on the interconnecting cable will be dependent on natural resonance conditions
associated with the cable and EUT interface circuit parameters.
A circuit diagram of the 50 ohm, charged line, pulse generator required by CS115 is shown in
Figure A-16. Its operation is essentially the same as impulse generators used to calibrate
measurement receivers except that the pulse width is much longer. A direct current power
supply is used to charge the capacitance of an open-circuited 50 ohm coaxial line. The high
voltage relay is then switched to the output coaxial line to produce the pulse. The pulse width is
dependent upon the length of the charge line. The relay needs to have bounce-free contact
operation.
The calibration fixture with terminations is a 50 ohm transmission line. Since the injection probe
is around the center conductor within the fixture, a signal is being induced in the loop formed by
the center conductor, the two 50 ohm loads, and the structure of the fixture to which the 50 ohm
loads are terminated. From a loop circuit standpoint, the two 50 ohm loads are in series,
providing a total loop impedance of 100 ohms. Because of the transmission line configuration,

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PULSE
RATE
CONTROL

VARIABLE
DC POWER
SUPPLY
HIGH VOLTAGE
COAXIAL RELAY

50 OHM COAXIAL
CHARGE LINE
50 OHM
COAXIAL
OUTPUT
CONNECTOR

50 OHM COAXIAL
OUTPUT LINE

FIGURE A-16. Circuit diagram of CS115 pulse generator.

inductance effects are minimized. Measurement of induced current levels is performed by

measuring a corresponding voltage across one of the 50 ohm loads. Since the 50 ohm loads are
in series for the induced signal, the total drive voltage is actually two times that being measured.
Paragraph 5.14.3.4b(3) of CS115 requires verification that the rise time, fall time, and pulse
width portions of the applied waveform are present in the observed waveform induced in the
calibration fixture. Figure A-17 shows a typical waveform that will be present. Since the
frequency response of injection probes falls off at lower frequencies, the trapezoidal pulse
supplied to the probe sags in the middle portion of the pulse that is associated with the lower
frequency content of the applied signal. The relevant parameters of the waveform are noted. It
is critical that an injection probe be used with adequate response at higher frequencies to produce
the required rise time and fall time characteristics.
As also specified in CS114, testing is required on both entire power cables and power cables
with the returns removed to evaluate common mode coupling to configurations which may be
present in different installations. In some installations, the power returns are routed with the
high side wiring. In other installations, power returns are tied to system structure near the
utilization equipment with system structure being used as the power return path.

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PULSE WIDTH MAINTAINED

AT > 30 NANOSECONDS

2
AMPERES

0
RISETIME AND FALLTIME
MAINTAINED AT < 2 NANOSECONDS
-2

-4

0 5 10 15 20 25 30 35 40
TIME (NANOSECONDS)

FIGURE A-17. Typical CS115 calibration fixture waveform.

RS06 was previously included in MIL-STD-462. RS06 was a formalization of the "chattering
relay" test used widely throughout the military aircraft industry. This test procedure improves on
RS06. The chattering relay has been found to be effective for determining upset conditions of
equipment. The basic concept was to electrically connect the relay coil in series with a normally
closed contact and allow the relay to continuously interrupt itself. The wire between the coil and
contact was used to couple the transient onto EUT cables. The greatest concern with the
chattering relay is that it does not produce a repeatable waveform since an arcing process is
involved. The particular relay being used and the condition of its contact and coil mechanics play
a large role. CS115 retains the most important characteristic of the chattering relay which is the
fast rise time waveform and also has the important advantage of a consistent excitation
waveform.
The same calibration fixture used for CS114 can be used for this test procedure. An available
design is shown in Figure A-9.

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A.5.15 (5.15) CS116, conducted susceptibility, damped sinusoid transients, cables and
power leads, 10 kHz to 100 MHz.
Applicability and limits: The requirements are applicable to all electrical cables interfacing
with each EUT enclosure and also individually on each power lead. The basic concept is to
simulate electrical current and voltage waveforms occurring in platforms from excitation of
natural resonances.
In contrast to CS115 that excites natural resonances, the intent of this requirement is to control
the waveform as a damped sine. Damped sine waveforms (sometimes complex combinations)
are a common occurrence on platforms from both external stimuli such as lightning and
electromagnetic pulse and from platform electrical switching phenomena. Waveforms appearing
on cables can be due to the cable itself resonating or to voltage and current drives resulting from
other resonances on the platform. Wide frequency coverage is included to account for a wide
range of conditions. Transients caused from switching actions within the platform can also
result in similar waveforms.
A consideration for the requirement is whether momentary upsets are allowable if the EUT is
capable of self-recovery to normal operation. Some upsets may occur that are not even noticed
by an operator due to self-correcting mechanisms in the equipment. There may be cases where
longer term upset is acceptable which may possibly require action by an operator to reset the
equipment. The EMITP should address any instances where the contractor proposes that
observable upsets be accepted.
A limited set of damped sine waves is specified to address a sampling of the various ringing
frequencies that may be present in the platform. An advantage of using a set of damped sine
waves is that different circuit types are evaluated for various waveform attributes that may cause
worst-case effects. Some circuits may respond to peak amplitude while others may respond to
total energy or rate of rise.
The requirement to test at resonant frequencies determined through loop circuit characterization
evaluation has been removed from this version of the standard. Test experience had shown that
equipment was no more susceptible at these frequencies than the standard frequencies.
The current limits are set at levels that cover most induced levels found in platforms during
system-level testing to external transient environments. The lower frequency breakpoints are at
worst-case platform resonant frequencies below which the response will fall off at 20 dB/decade.
The upper frequency breakpoint is located where the spectral content of the transient
environments falls off.
Possible tailoring of the requirements by the procuring activity in contractual documents is
adjustment of the curve amplitude either higher or lower based on the degree of protection
provided in the area of the platform where the equipment and interconnecting cabling will be
located. A caution with this particular requirement based on past experiences is that the platform
designer should be required to share in the burden of the hardening process by providing stress
reduction measures in the platform. The equipment should not be expected to provide the total
protection. Protection against transients generated internal to the platform needs to remain a
consideration. Another potential tailoring area is adjusting the lower frequency breakpoint to be
more consistent with the lowest resonance of a particular platform.

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Test procedures: The calibration fixture with terminations is a 50 ohm transmission line. Since
the injection probe is around the center conductor within the fixture, a signal is being induced in
the loop formed by the center conductor, the two 50 ohm loads, and the structure of the fixture to
which the 50 ohm loads are terminated. From a loop circuit standpoint, the two 50 ohm loads
are in series, providing a total loop impedance of 100 ohms. Because of the transmission line
configuration, inductance effects are minimized. Measurement of induced current levels is
performed by measuring a corresponding voltage across one of the 50 ohm loads. Since the 50
ohm loads are in series for the induced signal, the total drive voltage is actually two times that
being measured.
In the past, MIL-STD-462 included test procedures CS10, CS11, CS12, and CS13, which
addressed various types of damped sine testing on both cables and individual circuits or
connector pins. This test procedure is a single replacement for all those procedures. CS116
addresses testing of cables (interconnecting including power) and individual power leads. The
common mode cable portion of the test is the best simulation of the type of condition present on
platforms from electromagnetic field excitation. The individual power lead test addresses
differential type signals present on platforms from switching functions occurring in the power
system.
As necessary, the test can be applied in a straightforward manner to wires on individual pins on
an EUT connector or to individual circuits (twisted pairs, coaxial cables, and so forth).
Since the quality factor (Q) of the damped sine signal results in both positive and negative peaks
of significant value regardless of the polarity of the first peak, there is no requirement to switch
the polarity of the injected signal.
The common mode injection technique used in this procedure and other procedures such as
CS114 is a partial simulation of the actual coupling mechanism on platforms. The magnetic
field in the injection device is present at the physical location of the core of the injection device.
In the platform, the electromagnetic field will be distributed in space. The injection probe
induces a voltage in the circuit loops present with the voltage dropping and current flowing
based on impedances present in the loop. There is a complex coupling relationship among the
various individual circuits within the cable bundle. The injection probe is required to be close to
the EUT connector for standardization reasons to minimize variations particularly for higher
frequencies where the shorter wavelengths could affect current distribution.
Exercise caution to ensure that attenuators and current injection probes are rated such that they
will not be damaged nor have their characteristics altered by the injected signals. Attenuators
are generally rated in terms of their ability to handle average power. The peak power and
voltages associated with the injected susceptibility signal can damage attenuators. For example,
the 10 A current limit for CS116, exposes the attenuator to 500 V (10 A x 50 ohms) levels,
which corresponds to a peak power of 5 kW ((500 V)2/50 ohms). Similarly, current injection
probes can have their magnetic properties altered by the pulsed signals.
For measurement of Q of the injected waveform, Figure CS116-1 specifies the use of the peak of
the first half-sine wave and the associated peak closest to being 50% down in amplitude. Some
facilities use a damped cosine waveform rather than a damped sine. Since this waveform is more
severe than the damped sine because of the fast risetime on the leading edge, there is no
prohibition from using it. Because of potential distortion caused by leading edge effects, the first

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peak should not be used to determine Q for damped cosine waveforms. The next half peak
(negative going) should be used together with the associated negative peak closest to 50% down.
Equipment may exhibit failures with this waveform that would not be present with the damped
sine.
A.5.16 (5.16) RE101, radiated emissions, magnetic field, 30 Hz to 100 kHz.
Applicability and limits: This requirement is specialized and is intended primarily to control
magnetic fields for applications where equipment is present in the installation which is
potentially sensitive to magnetic induction at lower frequencies. The most common example is a
tuned receiver that operates within the frequency range of the test.
RS101 is a complimentary requirement imposed on equipment to ensure compatibility with the
anticipated magnetic fields. The RS101 limits are higher to allow for variations in performance
between manufactured items and to account for the possibility that the emissions from the EUT
may couple into a larger physical area than that evaluated under the RS101 test procedures.
The Navy RE101 limit is based on preventing induction of more than 0.5 μV (nominal) in an
RG-264A/U transmission line (loop area, A, of 0.65 square inches), with a maximum induced
level of 4 μV at 60 Hz. The need to limit the low frequency magnetic field emissions from
equipment is due to the close proximity of electronic and electrical systems and associated cables
installed on the Navy platforms, and the essentiality of low frequency sensors and systems. The
primary concerns are potential effects to low frequency acoustic systems and sensors, and ELF
and VLF/LF communications systems and sensors that have sensitivities in the nV range.
Note that the limit does not take into account magnetic effects from equipment such as magnetic
launchers, magnetic guns and the like.
An estimate can be made of the types of induced levels that will result in circuitry from the
limits. Magnetic fields act by inducing voltages into loop areas in accordance with Faraday's
law (V = -dφ/dt). For a uniform magnetic field perpendicular to the loop area, the induced
voltage from Faraday's law reduces to V = -2πfBA.
f = Frequency of Interest B = Magnetic Flux Density A = Loop Area
The Army RE101 limit is based on preventing induction of more than 2.5 mV (5 mV for RS101)
in a 12.7 cm (5 inch) diameter loop. Since magnetic induction is proportional to frequency and
the limit falls off at 20 dB/decade, the induced voltage in a given loop area is constant. Since the
Army limit is greater than or equal to the Navy limit at all frequencies, this induced level
represents the worst-case. The primary concerns are potential effects to engine, flight and
weapon turret control systems and sensors that have sensitivities in the mV range.
There are certain limited applications in the Air Force where an RE101 requirement needs to be
considered. These applications are primarily when a subsystem will be installed in an aircraft in
close proximity to an antenna connected to a VLF/LF receiver. An appropriate limit needs to be
chosen based upon distances between the equipment and the antenna.
For Army applications, possible tailoring is increasing the limit for single-use equipment that
will be located a sufficient distance from any potentially susceptible systems or waiving of the
requirement.

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Test procedures: A 13.3 cm loop is specified for the test.

If the maximum level is always observed on one face or on one cable at all frequencies, then data
only needs to be recorded for that face or cable.
Typical points of magnetic field emissions leakage from EUT enclosures are CRT yokes,
transformers and switching power supplies.
MIL-STD-462D required measurement of emissions from electrical interface cables. This
standard limits measurements to electrical interface connectors. This change recognizes that the
connectors are the most likely place for emissions associated with electrical interfaces to occur
due to a number of reasons. One is that signal paths transition from normal cable construction
techniques (such as twisted pairs) to parallel routing through the connector pins. Also, there are
potential contributions from shield termination techniques.
A possible alternative measurement tool in this frequency range is wave analyzer using a Fast
Fourier Transform algorithm. Use of this type of instrumentation requires specific approval by
the procuring activity.
A generic correction factor curve was included in MIL-STD-462D to convert from the voltage
indicated by the measurement receiver to the magnetic field in dBpT. However, the various
manufacturers use different construction techniques that cause the actual factor to vary
somewhat. Therefore, it is necessary to use the manufacturers’ supplied data.
Measurements are now required for each point of maximum radiation which exceeds the RE101
limit at 7 cm. These measurements are performed by increasing the measurement distance until
the emission falls below the specified limit. The fall-off measurement data is intended to assist
the equipment designer in determining the source of the magnetic field emissions and in the
development of appropriate mitigation techniques. It should be noted the EUT is required to
comply with the applicable RE101 limit at 7cm; this is not a change to the RE101 limit or
measurement distance.
A.5.17 (5.17) RE102, radiated emissions, electric field, 10 kHz to 18 GHz.
Applicability and limits: The requirements are applicable to electric field emissions from the
EUT and associated cables. The basic intent of the requirement is to protect sensitive receivers
from interference coupled through the antennas associated with the receiver. Many tuned
receivers have sensitivities on the order of 1 μV and are connected to intentional apertures (the
antenna) that are constructed for efficient reception of energy in the operating range of the
receiver. The potential for degradation requires relatively stringent requirements to prevent
platform problems.
There is no implied relationship between this requirement and RS103 that addresses radiated
susceptibility to electric fields. Attempts have been made quite frequently in the past to compare
electric field radiated emission and susceptibility type requirements as a justification for
deviations and waivers. While RE102 is concerned with potential effects with antenna-
connected receivers, RS103 simulates fields resulting from antenna-connected transmitters.
Often, the same equipment item will be involved in influencing both requirements. A 30 watt
VHF-AM radio with a typical blade antenna operating at 150 MHz can easily detect a 40
dBμV/m electric field (approximately -81 dBm developed at receiver input) while in the receive

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mode. When this same piece of equipment transmits at the same 150 MHz frequency, it will
produce a field of approximately 150 dBμV/m (32 V/m) at a 1 meter distance. The two field
levels are 110 dB apart.
The limit curves are based on experience with platform-level problems with antenna-connected
receivers and the amount of shielding typically between antennas and equipment and associated
wiring. The limits for surface ships, both topside and below decks, is based on numerous
documented incidents of case and cable radiation coupling to receiver antennas and sensitive
systems. The topside limit is more stringent than corresponding electric field radiation emissions
requirements contained in military-related international agreements and standards such as those
used by NATO. The below deck limit is comparable to many commercial/international
standards.
For submarines, the RE102 limit distinguishes between equipment located internal versus
external to the pressure hull. For equipment located external to the pressure hull, stricter limits
are imposed. Possible tailoring is to apply the external RE102 requirement only to equipment
that is located above the waterline.
The limit curves for equipment in internal installations on fixed wing aircraft are placed for air
vehicles that are not designed to have intentionally shielded volumes that are effective across the
frequency range of the test. Some minimal shielding is present. The curve for equipment in
external installations and helicopters is 10 dB more stringent because even this minimal
shielding is not available.
These limits for the 30 to 400 MHz band, in particular, have been validated as being properly
placed. It has become standard practice on some aircraft programs to use spectral analysis
equipment wired to aircraft antennas to assess degradation due to radiated emissions from
onboard equipment. Many problems due to out-of-limit conditions in this band have been
demonstrated. It has also been determined that equipment meeting the limit generally does not
cause problems. Most of this experience is on fighter size aircraft. The 20 dB/decade increase
in the limit above 100 MHz is due to the aperture size of a tuned antenna (Gλ2/(4π)) decreasing
with frequency. The coupled power level from an isotropic tuned antenna will remain constant.
The curve breaks at 100 MHz because of difficulty with maintaining a tuned antenna due to
increasing physical size and the lower likelihood of coupling to the antenna with longer
wavelengths.
No limit is specified below 2 MHz for internal equipment on fixed-wing aircraft. There are
antennas on some aircraft that operate below 2 MHz; however, these antennas are usually
magnetic loops that have an electrostatic shield. These antennas have very short electrical
lengths with respect to the wavelength of frequencies below 2 MHz and any electric field
coupling will be inefficient. With the exception of helicopters, there is no known history of
coupling problems to these antennas or to cabling, despite substantial above limit conditions with
respect to past MIL-STD-461 requirements. The inefficient coupling to cabling at lower
frequencies has been demonstrated innumerable times in EMI testing.
The limits for Navy mobile and all Army ground equipment are the same. Also, the limits for
Navy fixed and all Air Force ground equipment are identical. The 20 dB difference between the
limits exists because of the general situations where the equipment is deployed. The Navy
mobile is primarily oriented toward the Marines that operate in a fashion similar to the Army.

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Equipment is often very close to unprotected antennas such as installations in vehicles or tents or
near physically small helicopter aircraft. The Navy fixed and most Air Force installations have
less critical coupling situations with regard to antenna coupling.
The limit for surface ships is based on numerous documented incidents of case and cable
radiation coupling to receiver antennas. The use of hand-held type transceivers below deck
within a ship is increasing and can be plagued by excessive levels of interference below deck.
The limit is more stringent than corresponding electric field radiation emissions requirements
contained in military-related international agreements and standards such as those used by
NATO.
Another issue is that there have been substantial conflicts between allowed radiated levels
implied by the power quality limits of MIL-STD-704 and previous MIL-STD-461 requirements.
For example, MIL-STD-704 allows approximately 0.63 Vrms on 115 V, 400 Hz, AC power buses
at 15 kHz. Based on laboratory testing, this level will radiate at approximately 76 dBμV/m.
This level is 31 dB above the previous MIL-STD-461 limit for aircraft equipment. It is
interesting to note that if the rod antenna in the MIL-STD-462 setup were usable down to 400
Hz, an approximate 1 V/m level would be indicated because of the power source waveform.
Possible tailoring by the procuring activity for contractual documents is as follows. The limits
could be adjusted based on the types of antenna-connected equipment on the platform and the
degree of shielding present between the equipment, associated cabling, and the antennas. For
example, substantial relaxations of the limit may be possible for equipment and associated
cabling located totally within a shielded volume with known shielding characteristics. It may be
desirable to tailor the frequency coverage of the limit to include only frequency bands where
antenna-connected receivers are present. Some caution needs to be exercised in this regard
since there is always the chance the equipment will be added in the future. For example, it is not
uncommon to add communications equipment (such as HF radio) onboard an aircraft as different
missions evolve.
Based on the above discussion concerning MIL-STD-704, relaxing of RE102 limits for aircraft
should be considered at lower frequencies for power generation equipment to avoid conflicts
between the two sets of requirements.
Test procedures: Specific antennas are required by this test procedure for standardization
reasons. The intent is to obtain consistent results between different test facilities.
In order for adequate signal levels to be available to drive the measurement receivers, physically
large antennas are necessary. Due to shielded room measurements, the antennas are required to
be relatively close to the EUT, and the radiated field is not uniform across the antenna aperture.
For electric field measurements below several hundred megahertz, the antennas do not measure
the true electric field.
The 104 cm rod antenna has a theoretical electrical length of 0.5 meters and is considered to be a
short monopole with an infinite ground plane. It would produce the true electric field if a
sufficiently large counterpoise were used to form an image of the rod in the ground plane.
However, there is not adequate room. The biconical and double ridged horn antennas are
calibrated using far-field assumptions at a 1 meter distance. This technique produces

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standardized readings. However, the true electric field is obtained only above approximately 1
GHz where a far field condition exists for practical purposes.
The defined configuration for rod antennas measurements in Figure RE102-5 came from a study
of various approaches to obtaining the most accurate results. A calibrated vertical field was first
generated using a special structure and was measured with an electrically small broadband
sensor (RS103) in an empty room, with the sensor located at the center position of the rod. The
rod antenna was then placed at its normal location and a field level indicated by the rod antenna
was measured (scaled to prevent saturation). Bonding the counterpoise to the bench ground
plane or the floor with a wide strap was found to enhance readings at higher frequencies of the
rod and depress readings at other frequencies. Floating the counterpoise with the coaxial cable
electrically bonded at the floor with a weak ferrite sleeve (lossy with minimum inductance) on
the cable produced the best overall results. Lowering the antenna such that the center point of
the rod is 120 cm above the floor to be consistent with the other antennas improved the results
further.
For shielded enclosures that do not have an available point for bonding the coaxial cable from
the matching network to the floor directly beneath the counterpoise, a low inductance copper
sheet should be installed from the nearest access point on the floor to the counterpoise location.
Another issue is that some rod antennas have output connectors that are not electrically bonded
to the matching network enclosure. These antennas include a common choke that have the
return side of the connector wired through the choke. It is required that these antennas be
modified to bond the shell of the connector to the enclosure. This change does not affect the
antenna factor but can have a large affect on the resulting measurements.
Antenna factors are determined using the procedures of SAE ARP-958. They are used to
convert the voltage at the measurement receiver to the field strength at the antenna. Any RF
cable loss and attenuator values must be added to determine the total correction to be applied.
Previous versions of this standard specified conical log spiral antennas. These antennas were
convenient since they did not need to be rotated to measure both polarizations of the radiated
field. The double ridged horn is considered to be better for standardization for several reasons.
At some frequencies, the antenna pattern of the conical log spiral is not centered on the antenna
axis. The double ridged horn does not have this problem. The circular polarization of the
conical log spiral creates confusion in its proper application. Electric fields from EUTs would
rarely be circularly polarized. Therefore, questions are raised concerning the need for 3 dB
correction factors to account for linearly polarized signals. The same issue is present when spiral
conical antennas are used for radiated susceptibility testing. If a second spiral conical is used to
calibrate the field correctly for a circularly polarized wave, the question arises whether a 3 dB
higher field should be used since the EUT will respond more readily to linearly polarized fields
of the same magnitude.
Other linearly polarized antennas such as log periodic antennas are not to be used. It is
recognized that these types of antennas have sometimes been used in the past; however, they will
not necessarily produce the same results as the double ridged horn because of field variations
across the antenna apertures and far field/near field issues. Uniform use of the double ridge horn
is required for standardization purposes to obtain consistent results among different test
facilities.

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The stub radiator required by the procedure is simply a short wire (approximately 10 cm)
connected to the center conductor of a coaxial cable that protrudes from the end of the cable.
There are two different mounting schemes for baluns of available 104 cm rod antennas with
respect to the counterpoise. Some are designed to be mounted underneath the counterpoise
while others are designed for top mounting. Either technique is acceptable provided the desired
0.5 meter electrical length is achieved with the mounting scheme.
The 10 pF capacitor used with the rod antenna in 5.17.3.4c(3) as part of the system check
simulates the capacitance of the rod element to the outside world. With the rod antenna, the
electric field present induces a voltage in the rod that is applied to the matching network
circuitry. One of the functions of the matching network is to convert the high impedance input
of the antenna element to the 50 ohm impedance of the measurement receiver. The 10 pF
capacitor ensures that the correct source impedance is present during the check. Some antennas
have a 10 pF capacitor built into the rod balun for calibration purposes and some require that an
external capacitor be used.
For measurement system checks, establishing the correct voltage at the input to the 10 pF
capacitor can be confusing dependent upon the design of the antenna and the associated
accessories. Since, the electrical length of the 104 cm rod is 0.5 m, the conversion factor for the
induced voltage at the input to the 10 pF capacitor is 6 dB/m. If the limit at the measurement
system check frequency is 34 dBμV/m, the required field level to use for measurement system
check is 6 dB less than this value or 28 dBμV/m. The voltage level that must be injected is:
28 dBμV/m – 6 dB/m = 22 dBμV
Since the input impedance at the 10 pF capacitor is very high, a signal source must be loaded
with 50 ohms (termination load or measurement receiver) to ensure that the correct voltage is
applied. A “tee” connection is used with the signal source connected to the first leg, the 50 ohm
load connected to the second leg, and the center conductor of the third leg connected to the 10 pF
capacitor.
Accessories provided for rod antennas, such as calibration networks or voltage dividers, to assist
in signal injection and calibration have been found to have stray capacitance issues that produce
incorrect readings. The technique shown in Figure RE102-7 must be used. This same technique
should be used to determine calibration factors for the rod matching network. A network
analyzer signal output can be used to drive the 10 pF capacitor with the 50 ohm termination
connection routed to one of the analyzer receive ports (T) and the matching network routed to
the second receive port (R). With the analyzer operating in the mode to produce T/R, the
antenna factor is directly produced.
The stray capacitance issue mentioned above has also been found to result in incorrect factors
being supplied by organizations that calibrate rod antennas due to the use of incorrectly designed
calibration networks.
Some rod antennas include high pass filters that can be turned on and off by small switches
internal to the matching network. Caution should be exercised to ensure that the antennas factors
being used include the effect of any switches that are activated.

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The antenna positioning requirements in this procedure are based on likely points of radiation
and antenna patterns. At frequencies below several hundred MHz, radiation is most likely to
originate from EUT cabling. The 104 cm rod and biconical antennas have wide pattern
coverage. The equation in Figure RE102-7 is based on the rod and biconical being placed at
least every 3 meters along the test setup boundary. The double ridge horns have narrower
beamwidths. However, the shorter wavelengths above 200 MHz will result in radiation from
EUT apertures and portions of cabling close to EUT interfaces. The requirements for antenna
positioning above 200 MHz are based on including EUT apertures and lengths of cabling at least
one quarter wavelength.
All the specified antennas are linearly polarized. Above 30 MHz, measurements must be
performed to measure both horizontal and vertical components of the radiated field.
Measurements with the 104 cm rod are performed only for vertical polarization. This antenna
configuration is not readily adapted for horizontal measurements.
For equipment or subsystems that have enclosures or cabling in various parts of a platform, data
may need to be taken for more than one configuration. For example, in an aircraft installation
where a pod is located outside of aircraft structure and its associated cabling is internal to
structure, two different limits may be applicable. Different sets of data may need to be generated
to isolate different emissions from the pod housing and from cabling. The non-relevant portion
of the equipment would need to be protected with appropriate shielding during each evaluation.
A.5.18 (5.18) RE103, radiated emissions, antenna spurious and harmonic outputs, 10 kHz
to 40 GHz.
Applicability and limits: The requirements are essentially identical with CE106 for
transmitters in the transmit mode. There are no requirements for receivers or transmitters in the
standby mode. Most of the discussion under CE106 also applies to RE103. A distinction
between the requirements is that RE103 testing includes effects due to antenna characteristics.
The test itself is considerably more difficult.
Test procedures: Since the test procedure measures emissions radiating from an antenna
connected to a controlled impedance, shielded, transmission line, the measurement results should
be largely independent of the test setup configuration. Therefore, it is not necessary to maintain
the basic test setup described in the main body of this standard.
The test procedure is laborious and will require a large open area to meet antenna separation
distances. Equations in the test procedure specify minimum acceptable antenna separations
based on antenna size and operating frequency of the EUT. Antenna pattern searches in both
azimuth and elevation are required at the spurious and harmonic emissions to maximize the level
of the detected signal and account for antenna characteristics.
Sensitivity of the measurement system may need enhancement by use of preamplifiers and the
entire test needs to be coordinated with local frequency allocation authorities. All recorded data
has to be corrected for space loss and antenna gain before comparisons to the limit.
As shown in Figures RE103-1 and RE103-2, shielding might be necessary around the
measurement system and associated RF components to prevent the generation of spurious
responses in the measurement receiver. The need for such shielding can be verified by

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comparing measurement runs with the input connector of the measurement receiver terminated
in its characteristic impedance and with the EUT in both transmitting and stand-by modes or
with the EUT turned off. Also, the receiving or transmit antenna may be replaced with a dummy
load to determine if any significant effects are occurring through cable coupling.
The RF cable from the receive antenna to the measurement receiver should be kept as short as
possible to minimize signal loss and signal pick-up.
The band-rejection filters and networks shown in Figures RE103-1 and RE103-2 are needed to
block the transmitter fundamental and thus reduce the tendency of the measurement receiver to
generate spurious responses or exhibit suppression effects because of the presence of strong out-
of-band signals. These rejection networks and filters require calibration over the frequency
range of test.
Some caution needs to be exercised in applying Table II of the main body of this standard. In
5.18.3.4d(4) of the test procedure, a power monitor is used to measure the output power of the
EUT. In conjunction with the antenna gain, this value is used to calculate the effective radiated
power (ERP) of the equipment. In 5.18.3.4d(5) of the test procedure, the measurement receiver
is used to measure the power from a receiving antenna. This result is also used to calculate an
ERP. For the two measurements to be comparable, the measurement receiver bandwidth needs
to be sufficiently large to include at least 90% of the power of the signal present at the tuned
frequency. If the bandwidth in Table II of the main body of the standard is not appropriate, a
suitable measurement receiver bandwidth should be proposed in the EMITP.
For measurement of the magnitude of harmonic and spurious emissions with respect of the
fundamental, the bandwidths of Table II will normally produce acceptable results, regardless of
whether the bandwidth is large enough to process 90% of the power. Since the signal
bandwidth of harmonic and spurious emissions is usually the same as the fundamental, use of a
common bandwidth for measuring both the fundamental and the emissions will provide a correct
relative reading of the amplitudes.
A.5.19 (5.19) RS101, radiated susceptibility, magnetic fields, 30 Hz to 100 kHz.
Applicability and limits: This requirement is specialized and intended primarily to ensure that
performance of equipment potentially susceptible to low frequency magnetic fields is not
degraded. RE101 is a complimentary requirement governing the radiated magnetic field
emissions from equipment and subsystems. The RE101 discussion is also applicable to this
requirement.
The Navy RS101 limit was established by measurement of magnetic field radiation from power
distribution components (transformers and cables), and the magnetic field environment of Navy
platforms. The Navy RS101 limit from 30 Hz to 2 kHz was derived from the worst case
magnetic field radiation from a power transformer (~170 dBpT) and applicable cable types
(DSGU-400), and takes into account the user equipment power line harmonic content and
maximum anticipated power consumption. The Navy RS101 limit above 2 kHz is based on the
measured magnetic field environment of Navy platforms.
In past versions of this standard, the Navy RS101 and RE101 limits had the same general shape
with the RS101 limit being higher than the RE101 limit. In this version, there is a deviation

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from this pattern where the difference between the two limits is greater in some regions than in
the past. This change is due to a recognition that there are localized areas on the platforms
where there are sources of higher level magnetic fields that must be tolerated. The acceptance of
these higher levels within the platform is not justification for overall relaxation of the RE101
limit. Also, there is the possibility that the emissions from the EUT may couple into a larger
physical area than that evaluated under the RS101 test procedure.
The Army has maintained the basic relationship of the RS101 and RE101 limits having the same
shape. The RS101 limit is based on 5 mV (independent of frequency) being induced in a 12.7
cm (5 inch) diameter loop.
Test procedures: Laboratory tests have been performed to assess the possibility of using the
13.3 cm loop sensor specified in the RE101 test procedure instead of the 4 cm loop sensor used
in this test procedure to verify the radiated field. The testing revealed that the 13.3 cm loop
sensor did not provide the desired result due to variation of the radiated field over the area of the
loop sensor. Due to its smaller size, the 4 cm loop sensor provides an accurate measure of the
field near the axis of the radiating loop. A generic correction factor curve was included in MIL-
STD-462D to convert from the voltage indicated by the measurement receiver to the magnetic
field in dBpT. However, the various manufacturers use different construction techniques that
cause the actual factor to vary somewhat. Therefore, it is necessary to use the manufacturers’
supplied data.
The primary test procedure requires that testing be performed at each electrical interface
connector. On some small size EUTs, connectors may be closely spaced such that more than one
connector can be effectively illuminated for a particular loop position. The EMITP should
address this circumstance.
Helmholtz coils generate a relatively uniform magnetic field that is more representative of the
environment experienced on some platforms, particularly submarines. For this reason, the AC
Helmholtz coil test option is preferred for submarine applications. In addition to providing a
more realistic test bed, Helmholtz coils will, in general, reduce test time. Application of the
guidelines and analytical expressions presented herein should enable users to design and
construct Helmholtz coils for RS101 testing.
AC Helmholtz coils may be designed in accordance with the following guidance.
a. A closed form solution for the magnetic flux density produced along the axis of a
series-driven system of two identical circular coils is:

μ NIr 2 ⎛ 1 1 ⎞
Bz = o ⎜ + ⎟
2
⎝ (
⎜ z2 + r2 ) 3/2
( 2
)
2 3/2 ⎟
(d − z) + r ⎠
where,
Bz = magnetic flux density, Teslas
μo = permeability of free space, Henrys/meter
N = number of turns (same for each coil)
I = current, Amperes
r = coil radius, meters

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d = coil separation, meters

z = distance along common axis, meters
For a standard Helmholtz coil configuration, d = r. At the center of the test volume (z =
r/2), the above expression can be simplified:

Bz ≈
(8.99 ×10 ) N I
−7

r
b. The coil impedance can be estimated using general expressions for an RL series circuit.
The dominant term for frequencies below 100 kHz is the coil inductance that is the sum
of each coil’s series inductance (L) and the mutual inductance (M) between the two
coils:
LTotal = 2(L + M)
where:
M = αN2r, α = 0.494 x 10-6 Henrys/meter
The series inductance can be estimated using the following expression for the external
inductance of a circular coil where the wire bundle cross section is circular in shape and
small relative to the coil radius:
⎡ ⎛ 16r ⎞ ⎤
L = N 2 rμ0 ⎢ln⎜ ⎟ − 2⎥
⎣ ⎝ a ⎠ ⎦
where: a = diameter of wire bundle cross section, meters
There are several practical limitations that must be considered when designing AC Helmholtz
coils.
a. The coil drive current is limited by coil impedance. The dominant term in the coil
impedance is the coil inductive reactance. Because it is proportional to the square of
the number of turns (N), the coils should be designed with a minimum number of turns
needed to meet the low frequency test limit. Depending on coil size, it may be
necessary to construct the coils with one or more taps so the number of turns can be
reduced at higher frequencies.
b. The coil self-resonant frequency must be greater than 100 kHz. At self-resonance, it
may not be practical to generate sufficient drive current to achieve the test limit.
c. A series voltage drop will exist across each coil that is proportional to the product of the
coil impedance and coil drive current. Because the voltage drops are separated in space
by the distance between the coils, a voltage gradient will exist (electric field in V/m).
This field is maximum near the perimeter of circular coils. If the EUT is relatively
small compared to the available test volume, this effect may not be a concern.
However, if the EUT is near the coil perimeter, or if the electric field magnitude is
significant relative to the RS103 electric field susceptibility requirement, then steps
should be taken to minimize the electric field.

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It may not be practical using commonly available laboratory power amplifiers to achieve the
RS101 test limit for coils much larger than 4 feet in diameter. Consideration should be given to
tailoring the test limit if a larger Helmholtz coil is used. For example, it may be proposed that
the radiated test level exceed the limit by 3dB, rather than the 6 dB required for Helmholtz coils.
Any tailoring requires approval from the procuring activity.
Prior to initial use, the coils must be tested to ensure they are capable of generating the required
magnetic flux densities from 30 Hz to 100 kHz. Sufficient margin (2-3 dB) should be available
to compensate for the potential loading effect of nearby metallic structures or magnetic material.
It must be confirmed that the first indication of self-resonance appears above the RS101 upper
frequency limit of 100 kHz. For frequencies above 10 kHz, the magnitude of the electric field
component in the test volume should be determined either by direct measurement, or it should be
approximated by measuring the voltage drop across the coils and dividing by coil separation
distance. Unless the electric field component is much less than the RS103 electric field
susceptibility limit, the coils should be enclosed in a non-continuous electrostatic shield to
prevent ambiguity when interpreting susceptibility test results.
A.5.20 (5.20) RS103, radiated susceptibility, electric field, 10 kHz to 40 GHz.
Applicability and limits: The requirements are applicable to both the EUT enclosures and EUT
associated cabling. The basic concern is to ensure that equipment will operate without
degradation in the presence of electromagnetic fields generated by antenna transmissions both
onboard and external to the platform.
There is no implied relationship between this requirement and RE102. The RE102 limit is
placed primarily to protect antenna-connected receivers while RS103 simulates fields resulting
from antenna transmissions.
The limits specified for different platforms are simply based on levels expected to be
encountered during the service life of the equipment. They do not necessarily represent the
worst-case environment to which the equipment may be exposed. RF environments can be
highly variable, particularly for emitters not located on the platform. The limits are placed at
levels that are considered to be adequate to cover most situations, including design levels for
“back door” effects (excluding direct coupling to platform antennas or externally mounted
devices) resulting from RF high power threat emitters. The aircraft carrier hanger deck is not a
totally enclosed area. Investigation of the electromagnetic environment in the aircraft carrier
hangar deck on 9 aircraft carriers showed levels in the HF band (2 to 30 MHz) up to 42 V/m.
Therefore, equipment located in the hanger deck is required to meet the same 50 V/m level as
equipment in non-metallic ships (below decks) from 2 to 30 MHz.
An example which demonstrates the variability of environments for ground installations and the
need for effective tailoring of requirements is the installation of equipment in a large ground-
based radar facility. Some of these facilities transmit power levels over one megawatt and the
back lobes from the antennas can be substantial. Suitable design levels for equipment that will
be used in the facility or nearby need to be imposed.
For aircraft and ships, different limits are specified depending on whether the equipment receives
protection from platform structure. This distinction is not made for Army ground systems, such

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as tanks, because the same equipment used inside a structure is often used in other applications
where protection is not available.
The 200 V/m requirement for Army aircraft regardless of the location or criticality of the
equipment is based on the use of Army aircraft. Portions of the external environment accepted
for most of the Army's aircraft is higher than 200 V/m. Army aircraft, especially rotary wing,
have flight profiles that are almost exclusively nap-of-the-earth (NOE). The NOE profiles allow
for much closer and longer duration encounters with high power emitters. This approach is
similar to the FAA approach that recommends that Visual Flight Rules (VFR) helicopters be
qualified to levels higher than fixed wing aircraft.
For submarines, the RS103 limit now distinguishes between equipment located internal versus
external to the pressure hull. For equipment installed internal to the pressure hull, 10 V/m is
now specified above 30 MHz to account for portable transmitters used within the submarine.
For equipment located external to the pressure hull, stricter limits are imposed to more closely
reflect the electromagnetic environment. The external RS103 limits should be applied only to
equipment that is required to be fully operational when located above the waterline. Separate
limits are specified, which are less severe, for equipment that is “external” to the pressure hull
but located with the submarine superstructure (metallic boundary).
Using circularly polarized fields is not allowed due to problems with using the spiral conical
antennas specified in versions of MIL-STD-462 in the past. Circularly polarized fields were
convenient since they avoided the need to rotate a linearly polarized antenna to obtain both
polarizations of the radiated field. However, problems existed with this antenna. At some
frequencies, the antenna pattern of the conical log spiral is not centered on the antenna axis.
Also, the circular polarization of the conical log spiral creates confusion in its proper application.
The EUT and associated cabling can be expected to respond more readily to linearly polarized
fields. If a second spiral conical were used to calibrate the field radiated from the first spiral
conical antenna, it would indicate an electric field 3 dB higher than a linearly polarized antenna.
The question arises whether a 3 dB higher field should be used for a spiral conical transmit
antenna to obtain response characteristics similar to a linearly polarized field. Similarly, if a
spiral conical antenna were used to calibrate a linearly polarized field, the indication would be 3
dB below the true electric field strength.
Possible tailoring by the procuring activity for contractual documents is to modify the required
levels and required frequency ranges based on the emitters on and near a particular installation.
Actual field levels can be calculated from characteristics of the emitters, distances between the
emitters and the equipment, and intervening shielding. MIL-HDBK-235 provides information
on land, air, and sea based RF emitters, both hostile and friendly, which contribute to the overall
electromagnetic environment. The possible use of the equipment in other installations and the
potential addition or relocation of RF emitters needs to be considered. Other possible tailoring is
to change from the standard 1 kHz, square wave modulation or use additional modulations based
on actual platform environments.
RS103 requirements for surface ships and submarines are included at the tuned frequency of
antenna-connected receiver; there is no relaxation as for other platforms. The use of wireless
devices such as radio frequency identification (RFID) tags, handheld transceivers, wireless local
area network (WLAN), etc. is increasing rapidly for below decks applications. The requirement

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is to protect receivers at their tuned frequency, from the intentional emissions of wireless (RF
generating) devices used in close proximity to the receiver when sufficient isolation is provided
by the platform (for example, path loss from sea water between the emitter and receive antenna
for submarines) such that the receiver’s antenna does not detect significant levels from wireless
devices. The requirement is intended to ensure the equipment (receiver) does not respond to the
electric fields generated internal to the structure and is not to restrict signals received via the
antenna. The electric field strength at a distance of 1.0 m from a typical wireless device with an
effective isotropic radiated power (EIRP) of 100 mW (typical of 802.11 wireless LAN access
points, RFID, and wireless communications) is 1.73 V/m. Federal Communications Commission
(FCC) rules defines power limitations for WLANs in FCC Part 15.247 and requires effective
isotropic radiated power (EIRP) to be 1 W or less; this equates to an electric field strength of 5.5
V/m at a distance of 1 m. It should be noted that for fixed, point-to-point systems that use higher
gain directive antennas an EIRP of 4.0 W is permitted by the FCC.
Test procedures: Test facilities are permitted to select appropriate electric field generating
apparatus. Any electric field generating device such as antenna, long wire, TEM cell,
reverberating chamber (using mode tuned techniques) or parallel strip line capable of generating
the required electric field may be used. Fields should be maintained as uniform as possible over
the test setup boundary. Above 30 MHz, both horizontally and vertically polarized fields must
be generated. This requirement may limit the use of certain types of apparatus. Only vertically
polarized measurements are required below 30 MHz due to the difficulty of orienting available
test equipment for horizontal measurements.
Electric field sensors are located at least 30 cm above the ground plane below 1 GHz to
minimize electromagnetic boundary conditions of the ground plane affecting the field that is
present at the longer wavelengths. At and above 1 GHz, these effects are less pronounced and
the volumes being illuminated by antennas that typically have higher gain are smaller.
Therefore, the sensors need to be positioned in the main antenna beam and located at a height
where the EUT is being radiated.
The requirement to ensure that the E-field sensor is displaying the fundamental frequency is
primarily concerned with the biconical antenna, which has poor characteristics at the lower
frequencies. Harmonics, which are down from the fundamental in power, may radiate higher
levels than the fundamental due to the antenna being more efficient at the harmonic frequencies.
The primary way to avoid this effect is to use a transmission line radiator or a physically larger
transmit antenna at the lower frequencies (approximately below 70 MHz).
This version of the MIL-STD-461 allows larger distances than 1 meter between the transmit
antenna and the EUT boundary. This approach is actually preferable, where amplifier power is
available to obtain the required field, since more of the EUT is illuminated at one antenna
position.
Monitoring requirements emphasize measuring true electric field. While emission testing for
radiated electric fields does not always measure true electric field, sensors with adequate
sensitivity are available for field levels generated for susceptibility testing. Physically small and
electrically short sensors are required so that the electric field does not vary substantially over
the pickup element resulting in the measurement of a localized field. Broadband sensors not
requiring tuning are available.

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The use of more than one sensor is acceptable provided all sensors are within the beamwidth of
the transmit antenna. The effective field is determined by taking the average of the readings.
For example, if the readings of three sensors are 30, 22, and 35 V/m, the effective electric field
level is (30 + 22 + 35)/3 = 29 V/m.
Different sensors may use various techniques to measure the field. At frequencies where far-
field conditions do not exist, sensors must be selected which have electric field sensing elements.
Sensors that detect magnetic field or power density and convert to electric field are not
acceptable. Under far-field conditions, all sensors will produce the same result. Correction
factors must be applied for modulated test signals for equivalent peak detection as discussed
under 4.3.10.1. A typical procedure for determining the correction factor for these sensors is as
follows:
a. Generate a field at a selected frequency using an unmodulated source.
b. Adjust the field to obtain a reading on the sensor display near full scale and note the
value.
c. Modulate the field as required (normally 1 kHz pulse, 50% duty cycle) and ensure the
field has the same peak value. A measurement receiver with the peak detector selected
and receiving antenna can be used to make this determination.
d. Note the reading on the sensor display.
e. Divide the first reading by the second reading to determine the correction factor
(Subtract the two readings if the field is displayed in terms of dB).
f. Repeat the procedure at several frequencies to verify the consistency of the technique.
Above 1 GHz, radiated fields usually exhibit far-field characteristics for test purposes due to the
size of typical transmit antennas, antenna patterns, and distances to the EUT. Therefore, a
double ridged horn together with a measurement receiver will provide true electric field.
Similarly, the particular sensing element in an isotropic sensor is not critical, and acceptable
conversions to electric field can be made.
For equipment or subsystems that have enclosures or cabling in various parts of a platform, data
may need to be taken for more than one configuration. For example, in an aircraft installation
where a pod is located outside of aircraft structure and its associated cabling is internal to
structure, two different limits may be applicable. Different sets of data may need to be generated
to evaluate potential pod susceptibility due to coupling through the housing versus coupling from
cabling. The non-relevant portion of the equipment would need to be protected with appropriate
shielding.
Reverberating chambers, using mode tuned techniques, have been popular for performing
shielded effectiveness evaluations and, in some cases, have been used for radiated susceptibility
testing of equipment and subsystems. The concept used in reverberating chambers is to excite
available electromagnetic wave propagation modes to set up variable standing wave patterns in
the chamber. A transmit antenna is used to launch an electromagnetic wave. An irregular
shaped tuner is rotated to excite the different modes and modify the standing wave pattern in the
chamber. Any physical location in the chamber will achieve same peak field strength at some
position of the paddle wheel.

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Reverberation chambers have the advantage of producing relatively higher fields than other
techniques for a particular power input. Also, the orientation of EUT enclosures is less critical
since the all portions of the EUT will be exposed to the same peak field at some paddle wheel
position. The performance of a particular reverberation chamber is dependent upon a number of
factors including dimensions, Q of the chamber, number of available propagation modes, and
frequency range of use.
Some issues with reverberation chambers are as follows. The field polarization and distribution
with respect to the EUT layout are generally unknown at a point in time. If a problem is noted,
the point of entry into the EUT may not be apparent.
Reverberation chambers are sometimes treated as a good tool to determine potential problem
frequencies with conventional antenna procedures being used to evaluate areas of concern.
The performance of each chamber must be reviewed to determine the suitability of its use for
reverberation testing over a particular frequency range.
Reverberation chambers should be constructed in accordance with the following guidance in
order to function properly.
a. A tuner should be constructed of metal and installed with appropriate positioning
equipment to allow the tuner to be rotated 360 degrees in at least 200 evenly spaced
increments. The tuner should be constructed to be asymmetric with the smallest
dimension of the tuner being at least λ/3 of lowest frequency to be tested and the
longest dimension of the tuner being approximately 75% of the smallest chamber
dimension.
b. The enclosure should be free of any materials that might exhibit absorptive properties
such as tables, chairs, wood floors, sub-floors, shelves, and such. Support structures
should be constructed from high density foam.
c. Transmit and receive antennas should be at least 1.0 meter (λ/3 is the actual limitation)
from any wall or object and should be positioned to prevent direct alignment between
the main lobes of the two antennas or between the EUT and the main lobe of either
antenna.
d. The lower frequency limit is dependent on chamber size. To determine the lower
frequency limit for a given chamber, use one of the following methods:
(1) Using the following formula, determine the number of possible modes (N) which
can exist at a given frequency. If, for a given frequency, N is less than 100 then
the chamber should not be used at or below that frequency.
8π f 3
N = abd 3
3 c
where: a, b, and d are the chamber internal dimensions in meters
f is the operation frequency in Hz
c is the speed of propagation (3 x 108 m/s)

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(2) Use the methods detailed in IEC 61000-4-21 for determining the lowest useable
frequency based on field uniformity. Note: the MODE-TUNED calibration
procedure outlined in IEC 6100-4-21 may be substituted for the procedure
outlined in 5.19.4.4. Substitution of the data from the IEC procedure into the
equations of 5.19.4.4 is not allowed.
e. In order to assure that the time response of the chamber is fast enough to accommodate
pulsed waveform testing (other than the 1 kHz, 50% duty cycle, waveform specified),
determination of the chamber time constant must be accomplished using the following
procedure:
(1) Calculate the chamber Q using:

⎛ 16π 2V ⎞ ⎛ Pave rec ⎞

Q= ⎜ ⎟⎜ ⎟
⎝ η Txη Rx λ 3 ⎠ ⎜⎝ Pforward ⎟⎠

where ηTx and ηRx are the antenna efficiency factors for the Tx and Rx antennas
respectively and can be assumed to be 0.75 for a log periodic antenna and 0.9 for
a horn antenna, V is the chamber volume (m3), λ is the free space wavelength (m)
at the specific frequency, Pave rec is the average received power over one tuner
rotation, and Pforward is the forward power input to the chamber over the tuner
rotation at which Pave rec was measured.

(2) Calculate the chamber time constant, τ, using:

Q
τ=
2π f
where Q is the value calculated above, and f is the frequency (Hz)
(3) If the chamber time constant is greater than 0.4 of the pulse width of the
modulation waveform, absorber material must be added to the chamber or the
pulse width must be increased. If absorber material is added, repeat the
measurement and the Q calculation until the time constant requirement is satisfied
with the least possible absorber material. A new CLF ( f ) must be defined if
absorber material is required.
f. Prior to using the chamber, the effectiveness of the tuner should be evaluated at the
upper and lower frequencies to be used and at points between the endpoints not to
exceed 1 GHz spacing. To evaluate the stirring effectiveness, inject a CW signal into
the chamber at the desired frequency and record the net received power at 200 positions
of the tuner evenly spaced over a 360 degree rotation of the tuner. Determine the
correlation coefficient between the original set of received power and subsequent sets
obtained by rotating the last data point of the original set to the position of the first
point and then shifting all the other points to the right as depicted below.

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Original data D1, D2, D3, D4, D5, . . . D200

Shifted data (1) D200, D1, D2, D3, D4, . . . D199
Shifted data (2) D199, D200, D1, D2, D3, . . . D198
Shifted data (3) D198, D199, D200, D1, D2, . . . D197
Shifted data (4) D197, D198, D199, D200, D1, . . . D196
Shifted data (5) D196, D197, D198, D199, D200, D1, . . . D195
The correlation coefficient should drop to below 0.36 within five shifts of the data. This
will ensure that the tuner is operating properly. If the tuner fails this test, then the tuner
needs to be made either larger or more complex, or both.
g. National Bureau of Standards Technical Note 1092, “Design, Evaluation, and Use of a
Reverberation Chamber for Performing Electromagnetic Susceptibility/Vulnerability
Measurements” and National Institute of Standards and Technology Technical Note
1508, “Evaluation of the NASA Langley Research Center Mode-Stirred Chamber
Facility,” should be used as a guide in preparing a shielded room for reverberation
measurements.
A.5.21 (5.21) RS105, radiated susceptibility, transient, electromagnetic field.
Applicability and limits: This requirement is primarily intended for EUTs to withstand the fast
rise time, free-field transient environment of EMP. It applies for equipment enclosures which
are directly exposed to the incident field outside of the platform structure or for equipment inside
poorly shielded or unshielded platforms. This requirement may be tailored in adjustment of the
curve amplitude either higher or lower based on degree of field enhancement or protection
provided in the area of the platform where the equipment will be located. This requirement is
applicable only for EUT enclosures. The electrical interface cabling should be protected in
shielded conduit. Potential equipment responses due to cable coupling are controlled under
CS116.
Test procedures: To protect the EUT and actual and simulated loads and signal equipment, all
cabling should be treated with overall shielding; kept as short as possible within the test cell; and
oriented to minimize coupling to the EMP fields.
The EMP field is simulated in the laboratory using bounded wave TEM radiators such as TEM
cells and parallel plate transmission lines. To ensure the EUT does not significantly distort the
field in the test volume, the largest EUT dimension should be no more than a third of the
dimension between the radiating plates of the simulator. In these simulators the electric field is
perpendicular to the surfaces of the radiator. Since the polarization of the incident EMP field in
the installation is not known, the EUT must be tested in all orthogonal axes.
There is a requirement to first test at 10% of the specified limit and then increase the amplitude
in steps of 2 or 3 until the specified limit is reached for several reasons. This test has the
potential to burnout equipment and stating at lower levels provides a degree of protection. Also,
the equipment may exhibit susceptibility problems at lower test levels that do not occur at higher
test levels due to the presence of terminal protection devices (TPDs). At lower test levels, the

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 MIL-STD-461F
APPENDIX A

devices might not actuate resulting in higher stresses on circuits than for higher levels where
they do actuate.
Common mode signals can result on cables with inadequate isolation or leaky connectors in the
presence of radiated fields. A method of checking for potential problems is as follows:
a. Measure the E-field with the B-dot or D-dot probe.
b. Invert the probe by rotating it 180 degrees.
c. Measure the E-field again and invert the signal.
d. Overlay and subtract the two signals.
e. The result is the common mode signal.
If any significant level is present, corrections to the setup should be undertaken, such as
tightening of connectors and introduction of additional isolation, such as better shielded cables,
alternative routing, or shielding barriers.

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 MIL-STD-461F

CONCLUDING MATERIAL

Custodians: Preparing Activity:

Army: – AV Air Force: – 11
Navy: – AS (Project EMCS-2006-001)
Air Force – 11
DISA/JSC: – DC5

Review Activities
Army: – CR, MI, TE, AT, MD, MR
Navy: – SH, OS, EC, MC, CG, TD
Air Force: – 13, 19, 84, 99
NSA: – NS
DTRA: – DS

NOTE: The activities listed above were interested in this document as of the date of this
document. Since organizations and responsibilities can change, you should verify the currency
of the information above using the ASSIST Online database at http://assist.daps.dla.mil/.

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