Gemini RM
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).
Crew Size: 2. Habitable Volume: 2.55 m3. Structure: 638 kg (1,406 lb). Heat shield: 144 kg (317 lb). Reaction Control System: 133 kg (293 lb). Recovery Equipment: 98 kg (216 lb). Navigation Equipment: 62 kg (136 lb). Telemetry Equipment: 51 kg (112 lb). Electrical Equipment: 125 kg (275 lb). Communications Systems: 26 kg (57 lb). Crew Seats and Provisions: 426 kg (939 lb). Crew: 144 kg (317 lb). Miscellaneous Contingency: 99 kg (218 lb). RCS Fine No x Thrust: 16 x 98 N. RCS specific impulse: 283 sec. RCS total impulse: 90 kgf-sec. Electric System: 4.00 kWh. Battery: 180.00 Ah.
Related
- Family
- Manned spacecraft module
- Country
- USA
- Spacecraft
- Gemini
- Propellants
- N2O4/MMH