Apollo LM AS
Spacecraft · USA
Original archive entry. The text, images and links below are kept as they were written.
American manned spacecraft module. 10 launches, 1968.01.22 (Apollo 5) to 1972.12.07 (Apollo 17).
Crew Size: 2. Habitable Volume: 6.65 m3. Crew: 144 kg (317 lb). RCS Coarse No x Thrust: 16 x 440 N. RCS specific impulse: 290 sec. Spacecraft delta v: 2,220 m/s (7,280 ft/sec). Electric System: 17.00 kWh. Battery: 800.00 Ah.
Related
- Family
- Manned spacecraft module
- Country
- USA
- Spacecraft
- Apollo LM
- Propellants
- N2O4/Aerozine-50