Soyuz TMA-1[a], also catalogued as Soyuz TM-35, was a 2002 Soyuz mission to the International Space Station (ISS) launched by a Soyuz FG launch vehicle with a Russian-Belgian cosmonaut crew blasted off from the Baikonur Cosmodrome in Kazakhstan.[3] This was the fifth Russian Soyuz spacecraft to fly to the ISS. It was also the first flight of the TMA-class Soyuz spacecraft.[4] Soyuz TM-34 was the last of the prior Soyuz-TM spacecraft to be launched.

Soyuz TMA-1
TMA-1 approaches the ISS
Mission typeISS crew transport
OperatorRussian Space Agency
COSPAR ID2002-050A Edit this at Wikidata
SATCAT no.27552Edit this on Wikidata
Mission duration185 days, 22 hours, 53 minutes, 14 seconds
Orbits completed~3,020
Spacecraft properties
SpacecraftSoyuz-TMA-1 11F732 No. 211[1]
Spacecraft typeSoyuz-TMA
ManufacturerEnergia
Crew
Crew size3
LaunchingSergei Zalyotin
Frank De Winne
Yury Lonchakov
LandingNikolai Budarin
Kenneth Bowersox
Donald Pettit
CallsignYenisey
Start of mission
Launch dateOctober 30, 2002, 03:11:11 (2002-10-30UTC03:11:11Z) UTC
RocketSoyuz-FG
Launch siteBaikonur, Site 1/5
ContractorProgress
End of mission
Landing dateMay 4, 2003, 02:04:25 (2003-05-04UTC02:04:26Z) UTC
Landing siteKazakh Steppe (49°37′47″N 61°20′36″E / 49.62972°N 61.34333°E / 49.62972; 61.34333)
Orbital parameters
Reference systemGeocentric orbit
RegimeLow Earth orbit
Perigee altitude387 km (240 mi)
Apogee altitude395 km (245 mi)
Inclination51.63°
Period92.4 minutes
Epoch6 November 2002[2]
Docking with ISS
Docking portPirs nadir
Docking date1 November 2002, 05:01:20 UTC
Undocking date3 May 2003, 22:43:00 UTC
Time docked183 days, 17 hours, 41 minutes, 40 seconds

Launching mission insignia

Launching crew, from left: De Winne, Zalyotin and Lonchakov

Crew

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Position Launching crew Landing crew
Commander   Sergei Zalyotin, RSA
Second and last spaceflight
  Nikolai Budarin, RSA
Expedition 6 Soyuz Commander
Third and last spaceflight
Flight Engineer   Frank De Winne, ESA
First spaceflight
  Kenneth Bowersox, NASA
Expedition 6 ISS Commander/Soyuz Flight Engineer
Fifth and last spaceflight
Flight Engineer   Yury Lonchakov, RSA
Second spaceflight
  Donald Pettit, NASA
Expedition 6 Flight Engineer
First spaceflight

Mission parameters

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  • Mass: 7,220 kg (15,910 lb), gross
  • Perigee: 193 km
  • Apogee: 235 km
  • Inclination: 51.6°
  • Period: 88.7 minutes

Docking with ISS

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  • Docked to ISS: November 1, 2002, 05:01 UTC (to Pirs module)
  • Undocked from ISS: May 3, 2003, 22:43 UTC (from Pirs module)

Specifications

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Section ref: Astro[5]
  • Gross mass: 7,220 kg (15,910 lb).
  • Unfuelled mass: 6,320 kg (13,930 lb).
  • Height: 6.98 m (22.90 ft).
  • Diameter: 2.20 m (7.20 ft).
  • Span: 10.70 m (35.10 ft).
  • Thrust: 3.92 kN (881 lbf).
  • Specific impulse: 305 s.

Mission highlights

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In the spring of 2001, a taxi mission to the space station was being scheduled to take place in October 2002. At first the crew was to be commander Sergei Zalyotin and flight engineer Frank De Winne; however, a report released in February 2002 stated that American musician Lance Bass was interested in joining the crew for a one-week mission on board the Russian spacecraft. The mission began to fall through, and by September 2002 they had discontinued the training of Lance Bass due to the mission organizers' failure to meet the terms of the contract. They filled the vacant seat left by Lance Bass with Russian cosmonaut Yuri Lonchakov.

While the Soyuz TMA-1 was on orbit, the Space Shuttle Columbia disaster occurred and required a change in crew changeout process. The Soyuz system became the sole method for crew to launch to and return from the ISS until the space shuttle was returned to service in July 2005.

Soyuz TMA-1 disembarked from ISS on May 4, 2003 and immediately began its return to Earth, marking the first entry and descent for this Soyuz class. A technical malfunction caused the Soyuz control system to abandon the gentler controlled entry and descent and instead fall back to the harsher ballistic reentry and descent. This resulted in a steep and off target landing of the spacecraft. The craft landed 300 miles short of the planned area, and the crew was subjected to severe acceleration loads. Communication with the Soyuz was lost because one antenna was ripped off during descent, and two more did not deploy. [citation needed] The crew regained communications through an emergency transmitter after landing. Due to this event, future crews would be provided with a satellite phone to establish contact with recovery forces.

Subsequent Soyuz TMA missions were able to successfully execute controlled reentries until the Soyuz TMA-10 and Soyuz TMA-11 missions which both also reverted to ballistic descents.

Don Pettit, concerned that the film documenting his science experiments on the ISS would be damaged by space radiation before the next Shuttle could bring it home, decided to secure the film and other items in a 20-kilogram (44 lb) pack he placed on his chest during reentry. While a normal Soyuz entry involves 3 G's, the ballistic reentry subjecting the crew to over 8 G's. This extreme force made the pack feel like a 160-kilogram (350 lb) weight pressing down on Pettit's chest.[6][7] Pettit was left exhausted and reportedly dislocated a shoulder, but the space agencies downplayed the situation saying the astronauts were in good shape.[8]

References

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  1. ^ McDowell, Jonathan. "Launch Log". Jonathan's Space Page. Retrieved 9 November 2013.
  2. ^ McDowell, Jonathan. "Satellite Catalog". Jonathan's Space Page. Retrieved 9 November 2013.
  3. ^ Quest.NASA.gov Space report No.46 Archived 2008-09-17 at the Wayback Machine
  4. ^ RussianSpaceWeb.com: Soyuz TMA-1
  5. ^ Astronautix.com: Soyuz TMA Archived 2009-04-14 at the Wayback Machine
  6. ^ Manley, Scott (2024-09-13). Astronaut Don Pettit's First Spaceflight was Crazy - And He's Still Flying!. Retrieved 2024-09-24 – via YouTube.
  7. ^ "Soyuz TMA-1 ISS EP-4". www.astronautix.com. Retrieved 2024-09-24.
  8. ^ Marmur Astana, Maxim (May 4, 2003). "Station Crew Returns Safely To Earth After Nerve-Wracking Search". Space Daily. Agence France-Presse. Retrieved 2024-09-24.

Footnotes

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  1. ^ T – транспортный – Transportnyi – meaning transport,
    M – модифицированный – Modifitsirovannyi – meaning modified,
    A – антропометрический, – Antropometricheskii meaning anthropometric).
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