Apollo Direct RM
Spacecraft · USA
Original archive entry. The text, images and links below are kept as they were written.
American manned spacecraft module. Study 1961. The retrograde module supplied the velocity increments required during the translunar portion of the mission up to a staging point approximately 1800 m above the lunar surface.
Engine thrust could be throttled down to 1201 kgf.
Related
- Family
- Manned spacecraft module
- People
- McDonnell
- Country
- USA
- Engines
- RL-10A-3
- Spacecraft
- Apollo Direct 2-Man, Gemini Lunar Lander
- Propellants
- Lox/LH2
- Agency
- NASA