Official name SOYUZ-TMA 7M
Alternative name Soyuz TMA-07M
Cospar ID 2012-074A
Norad ID 39032
Launch date 2012-12-19
Launch site TTMTR
Launch vehicle Soyuz-FG
Country/Organization Russia
Type application Crewed spacecraft
RCS size LARGE
Decay date 2013-05-14
Shape Cyl + Cone + Sphere + 2 Pan
Mass (kg) 7100
Diameter (m) 2.7
Height (m) 7.9
Span (m^2) 10.6
Propulsion KTDU-80 (S5.80)
Power 2 deployable fixed solar arrays, batteries

The modified Soyuz TMA crewed spacecraft for transporting Crews to the ISS has been developed on the basis of a Soyuz TMA spacecraft. In the new version, the Argon-16 computer (introduced on Soyuz-T back in the 1970s) is replaced by the new TsVM-101 computer. The latter is a much more capable computer, is almost 10 times lighter (8.3 kg vs. 70 kg) and much smaller. The analogue telemetry system is also replaced by a smaller digital telemetry system called MBITS.

It is to provide rescue of the main crew of the station in emergency and delivery of visiting crews.

During the flight the spacecraft fulfills the following tasks:

  • delivery of a visiting crew consisting of up to three persons and small accompanying cargoes
  • constant availability of the spacecraft, attached to the station during its crewed flight, in the standby mode to be ready for emergency descent of the main crew onto the ground in case of hazardous situation on the station, cosmonaut illness or injury, etc. (assured crew return vehicle function);
  • planned descent of the visiting crew onto the ground;
  • returning to the ground, together with the crew, payloads of relatively low mass and volume
  • disposal of wastes from the station in the living compartment to be burned down in the atmosphere during descent.

During a pressure test, the descent module of vehicle №704 was damaged beyond repair. The descent module was replaced with the one, which was originally planned to be used in vehicle №707. This repaired vehicle received the serial number №704A and flew on the Soyuz-TMA 07M mission.

During the missions of both Soyuz-TMA 14M and Soyuz-TMA 17M, one of the solar arrays remained stuck after launch and deployed only during the docking with the ISS.

Satellite COSPAR Date LS Launch Vehicle Remarks
SOYUZ-TMA 1M 2010-052A 2010-10-07 TTMTR Soyuz-FG
SOYUZ-TMA 2M 2011-023A 2011-06-07 TTMTR Soyuz-FG
SOYUZ-TMA 3M 2011-078A 2011-12-21 TTMTR Soyuz-FG
SOYUZ-TMA 4M 2012-022A 2012-05-15 TTMTR Soyuz-FG
SOYUZ-TMA 5M 2012-037A 2012-07-15 TTMTR Soyuz-FG
SOYUZ-TMA 6M 2012-058A 2012-10-23 TTMTR Soyuz-FG
SOYUZ-TMA 7M 2012-074A 2012-12-19 TTMTR Soyuz-FG
SOYUZ-TMA 8M 2013-013A 2013-03-28 TTMTR Soyuz-FG
SOYUZ-TMA 9M 2013-025A 2013-05-28 TTMTR Soyuz-FG
SOYUZ-TMA 10M 2013-054A 2013-09-25 TTMTR Soyuz-FG
SOYUZ-TMA 11M 2013-061A 2013-11-07 TTMTR Soyuz-FG
SOYUZ-TMA 12M 2014-013A 2014-03-25 TTMTR Soyuz-FG
SOYUZ-TMA 13M 2014-031A 2014-05-28 TTMTR Soyuz-FG
SOYUZ-TMA 14M 2014-057A 2014-09-25 TTMTR Soyuz-FG
SOYUZ-TMA 15M 2014-074A 2014-11-23 TTMTR Soyuz-FG
SOYUZ-TMA 16M 2015-016A 2015-03-27 TTMTR Soyuz-FG
SOYUZ-TMA 17M 2015-035A 2015-07-22 TTMTR Soyuz-FG
SOYUZ-TMA 18M 2015-043A 2015-09-02 TTMTR Soyuz-FG
SOYUZ-TMA 19M 2015-076A 2015-12-15 TTMTR Soyuz-FG
SOYUZ-TMA 20M 2016-018A 2016-03-18 TTMTR Soyuz-FG