LLV L-I
Spacecraft · USA
Original archive entry. The text, images and links below are kept as they were written.
American manned spacecraft module. Study 1966. Lunar Orbit Insertion stage for placing LLV into lunar orbit. Propulsion 2 x RL10-A3 with N2O4/MMH thrusters for orientation, midcourse, and ullage. Lunar orbit insertion of Lunar Logistics Vehicle lander and payload.
Spacecraft delta v: 1,100 m/s (3,600 ft/sec).
Related
- Family
- Manned spacecraft module
- Country
- USA
- Spacecraft
- LLV
- Propellants
- Lox/LH2