Apollo Direct RM

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Apollo Direct RM

Part of Apollo CSM

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.

Status: Study 1961. Thrust: 117.86 kN (26,495 lbf). Gross mass: 24,393 kg (53,777 lb). Unfuelled mass: 2,833 kg (6,245 lb). Height: 5.00 m (16.40 ft). Diameter: 6.61 m (21.68 ft).

Engine thrust could be throttled down to 1201 kgf.

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.

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