Apollo SM
Spacecraft · USA
Original archive entry. The text, images and links below are kept as they were written.
American manned spacecraft module. 22 launches, 1964.05.28 (Saturn 6) to 1975.07.15 (Apollo (ASTP)).
Structure: 1,910 kg (4,210 lb). Electrical Equipment: 1,200 kg (2,600 lb). RCS Coarse No x Thrust: 16 x 440 N. RCS specific impulse: 290 sec. RCS total impulse: 3,517 kgf-sec. Spacecraft delta v: 2,804 m/s (9,199 ft/sec). Electric System: 670.00 kWh. Electric System: 6.30 average kW.
Related
- Family
- Manned spacecraft module
- Country
- USA
- Spacecraft
- Apollo CSM
- Propellants
- N2O4/UDMH