Gemini LORV SM
Spacecraft · USA
Original archive entry. The text, images and links below are kept as they were written.
American manned spacecraft module. Study 1967. Calculated mass based on mission requirements, drawing of spacecraft, dimensions of propellant tanks.
RCS Coarse No x Thrust: 16 x 440 N. Spacecraft delta v: 1,000 m/s (3,200 ft/sec).
Related
- Family
- Manned spacecraft module
- Country
- USA
- Spacecraft
- Gemini LORV
- Propellants
- N2O4/UDMH