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Apollo SM
Part of Apollo CSM Family
American manned spacecraft module. 22 launches, 1964.05.28 (Saturn 6) to 1975.07.15 (Apollo (ASTP)).

AKA: Service Module. Status: Operational 1964. Thrust: 97.86 kN (22,000 lbf). Gross mass: 24,523 kg (54,063 lb). Unfuelled mass: 6,110 kg (13,470 lb). Specific impulse: 314 s. Height: 7.56 m (24.80 ft). Diameter: 3.90 m (12.70 ft).

Structure: 1,910 kg (4,210 lb). Electrical Equipment: 1,200 kg (2,600 lb). RCS Coarse No x Thrust: 16 x 440 N. RCS specific impulse: 290 sec. RCS total impulse: 3,517 kgf-sec. Spacecraft delta v: 2,804 m/s (9,199 ft/sec). Electric System: 670.00 kWh. Electric System: 6.30 average kW.



Family: Manned spacecraft module. Country: USA. Spacecraft: Apollo CSM. Propellants: N2O4/UDMH.

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