Soyuz TMA Spacecraft Main Characteristics
Name of characteristic,
dimensions |
Value |
Remarks |
| 1. Spacecraft mass, kg |
до 7220
|
|
| 2. Descent module mass, kg |
~ 2900
|
|
| 3. Crew, persons |
2:3
|
|
|
4. Orbit parameters
- inclination, deg
- altitude, km
- of insertion
- during spacecraft docking
- during spacecraft descent
|
51.6
202/238*
up to 425
up to 460
|
*) Perigee/apogee
|
|
5. Geometrical characteristics of the spacecraft,
mm
- body length
- maximal diameter
- diameter of living compartments
- solar array span
|
|
|
|
6. Calculated mass of payload, kg
|
|
With a 3-person crew |
| 7. Flying life*, days |
200
|
*) including the autonomous flight time |
|
8. Touchdown speed, m/s
- with the main parachute system
maximum / nominal
- with the reserve parachute system
maximum / nominal
|
|
3.6 / 2.6 (via Soyuz ТМ)
6.1 / 4.3 (via Soyuz TM)
|
| 9. Launch Vehicle |
Soyuz FG
|
Developed for the Soyuz TMA spacecraft,
has passed flight testing during the Progress spacecraft
launches in the years 2001-2002.
|
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