Gemini AM
Spacecraft · USA
Original archive entry. The text, images and links below are kept as they were written.
American manned spacecraft module. 12 launches, 1964.04.08 (Gemini 1) to 1966.11.11 (Gemini 12).
Structure: 160 kg (350 lb). Reaction Control System: 200 kg (440 lb). RCS Coarse No x Thrust: 6 x 420 N. RCS specific impulse: 273 sec. Spacecraft delta v: 101 m/s (331 ft/sec).
Related
- Family
- Manned spacecraft module
- Country
- USA
- Spacecraft
- Gemini
- Propellants
- Solid