LLV L-II
Spacecraft · USA
Original archive entry. The text, images and links below are kept as they were written.
American manned spacecraft module. Study 1966. Landing stage for delivery of up to 13,400 kg payload from lunar orbit to lunar surface. Propulsion 2 x RL10-A3 with N2O4/MMH thrusters for orientation, midcourse, and ullage. Delivery of lunar base elements from lunar orbit to lunar surface.
Spacecraft delta v: 2,400 m/s (7,800 ft/sec).
Related
- Family
- Manned spacecraft module
- Country
- USA
- Spacecraft
- LLV
- Propellants
- Lox/LH2