Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
Apollo CM
Part of Apollo CSM Family
American manned spacecraft module. 22 launches, 1964.05.28 (Saturn 6) to 1975.07.15 (Apollo (ASTP)).

AKA: Command Module. Status: Operational 1964. Gross mass: 5,806 kg (12,800 lb). Unfuelled mass: 5,731 kg (12,634 lb). Height: 3.47 m (11.38 ft). Diameter: 3.90 m (12.70 ft).

Crew Size: 3. Habitable Volume: 6.17 m3. Structure: 1,567 kg (3,454 lb). Heat shield: 848 kg (1,869 lb). Reaction Control System: 400 kg (880 lb). Recovery Equipment: 245 kg (540 lb). Navigation Equipment: 505 kg (1,113 lb). Telemetry Equipment: 200 kg (440 lb). Electrical Equipment: 700 kg (1,540 lb). Communications Systems: 100 kg (220 lb). Crew Seats and Provisions: 550 kg (1,210 lb). Crew: 216 kg (476 lb). Miscellaneous Contingency: 200 kg (440 lb). Environmental Control System: 200 kg (440 lb). RCS Coarse No x Thrust: 12 x 410 N. RCS specific impulse: 290 sec. RCS total impulse: 257 kgf-sec. Electric System: 20.00 kWh. Battery: 1,000.00 Ah.



Family: Manned spacecraft module. Country: USA. Spacecraft: Apollo CSM.

Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
© 1997-2017 Mark Wade - Contact
© / Conditions for Use