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T R I 6 0 - 3 0 Turbojet Engine: Main Features

The TRI 60-30 turbojet engine is designed to meet the requirements of modern missile manufacturers. It has a proven windmill start capability and aims to minimize size, weight, and costs. New processing methods have optimized performance. It uses fuel lubricated bearings to simplify systems and maintenance. The engine can power the Apache A and Storm Shadow/Scalp EG missiles.

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Alex Karim
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2K views1 page

T R I 6 0 - 3 0 Turbojet Engine: Main Features

The TRI 60-30 turbojet engine is designed to meet the requirements of modern missile manufacturers. It has a proven windmill start capability and aims to minimize size, weight, and costs. New processing methods have optimized performance. It uses fuel lubricated bearings to simplify systems and maintenance. The engine can power the Apache A and Storm Shadow/Scalp EG missiles.

Uploaded by

Alex Karim
Copyright
© © All Rights Reserved
We take content rights seriously. If you suspect this is your content, claim it here.
Available Formats
Download as PDF, TXT or read online on Scribd
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TRI 60-30

TURBOJET ENGINE

The TRI 60-30 turbojet engine is designed to Main Features


respond to the increasingly complex require-
ments of modern-day missile manufacturers. Operating Envelope
Flight envelope - altitude 0 to 12,000 m
In designing the engine, Microturbo has retai - - speed < Mach 0.95
ned the basic hallmarks of its predecessors, i.e. Windmill start envelope - altitude 0 to 7,500 m
proven windmill start capability and minimum - speed Mach 0.7 to 0.9
size, weight, acquisition and life-cycle costs. Requirements
Fuel JP5, JP8
New aerothermodynamic data processing Performance (engine uninstalled SLS)
methods have optimised the performance of Maximum thrust 550 daN/1,210 lbt
the TRI 60-30 rotor components, providing the Specific fuel consumption < 1.15 kg/daN/h
highest thrust-to-diameter and thrust-to- Dimensions and weight
weight ratios available in this engine class. Overall length (with jet-pipe) 1071 mm
The use of fuel lubricated bearings simplifies the Maximum diameter 343 mm
associated systems and engine maintenance. Dry weight 66 kg
Applications
Apache A MBDA
Storm Shadow/Scalp EG MBDA

Values indicated on this document are not binding.© Microturbo - 2005

Microturbo
8, chemin du pont de Rupé - BP 62089 - 31019 Toulouse Cedex 2 - France
Tel. +33 (0)5 61 37 55 00 - Fax +33 (0)5 61 70 74 45

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