Apollo CM
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)).
Crew Size: 3. Habitable Volume: 6.17 m3. Structure: 1,567 kg (3,454 lb). Heat shield: 848 kg (1,869 lb). Reaction Control System: 400 kg (880 lb). Recovery Equipment: 245 kg (540 lb). Navigation Equipment: 505 kg (1,113 lb). Telemetry Equipment: 200 kg (440 lb). Electrical Equipment: 700 kg (1,540 lb). Communications Systems: 100 kg (220 lb). Crew Seats and Provisions: 550 kg (1,210 lb). Crew: 216 kg (476 lb). Miscellaneous Contingency: 200 kg (440 lb). Environmental Control System: 200 kg (440 lb). RCS Coarse No x Thrust: 12 x 410 N. RCS specific impulse: 290 sec. RCS total impulse: 257 kgf-sec. Electric System: 20.00 kWh. Battery: 1,000.00 Ah.
Related
- Family
- Manned spacecraft module
- Country
- USA
- Spacecraft
- Apollo CSM