Gemini LSRS LOIM
Spacecraft · USA
Original archive entry. The text, images and links below are kept as they were written.
American manned spacecraft module. Study 1966. Calculated mass based on mission requirements, drawing of spacecraft, dimensions of propellant tanks.
Spacecraft delta v: 3,200 m/s (10,400 ft/sec).
Related
- Family
- Manned spacecraft module
- Country
- USA
- Spacecraft
- Gemini Lunar Surface Rescue Spacecraft
- Propellants
- N2O4/UDMH