Gemini EM
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: 250 kg (550 lb). Reaction Control System: 60 kg (132 lb). Telemetry Equipment: 40 kg (88 lb). Electrical Equipment: 294 kg (648 lb). Miscellaneous Contingency: 75 kg (165 lb). Environmental Control System: 117 kg (257 lb). RCS Fine No x Thrust: 8 x 98 N. RCS specific impulse: 288 sec. RCS total impulse: 1,078 kgf-sec. Spacecraft delta v: 222 m/s (728 ft/sec). Electric System: 151.00 kWh. Electric System: 2.16 average kW.
Related
- Family
- Manned spacecraft module
- Country
- USA
- Spacecraft
- Gemini
- Propellants
- N2O4/MMH