CEV Spacehab CM
Spacecraft · USA
Original archive entry. The text, images and links below are kept as they were written.
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.
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.
Related
- Family
- Manned spacecraft module
- Country
- USA
- Spacecraft
- CEV Spacehab
- Propellants
- N2O/C3H8