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CEV Spacehab CM
Part of Orion CEV
American manned spacecraft module. Study 2005. A 10% enlargement of the Apollo capsule, this re-entry vehicle provided the minimum volume for four crew to make re-entry from lunar distances.

Status: Study 2005. Payload: 750 kg (1,650 lb). Gross mass: 6,000 kg (13,200 lb). Height: 3.00 m (9.80 ft). Diameter: 4.30 m (14.10 ft).

Crew seating consisted of a pilot forward, with a view through a rendezvous and docking window, and three crew aft. Total cabin volume was 9 cubic meters.

Crew Size: 4. RCS Coarse No x Thrust: 12 x 400 N. RCS Propellants: 112 kg (246 lb). RCS specific impulse: 290 sec. Electric System: 2.00 average kW.

Family: Manned spacecraft module. Country: USA. Spacecraft: CEV Spacehab. Propellants: N2O/C3H8.
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