Apollo LM DS (original) (raw)

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Apollo LM DS

Part of Apollo LM

American manned spacecraft module. 10 launches, 1968.01.22 (Apollo 5) to 1972.12.07 (Apollo 17).

AKA: Descent Stage. Status: Operational 1968. Thrust: 44.04 kN (9,901 lbf). Gross mass: 10,149 kg (22,374 lb). Unfuelled mass: 1,984 kg (4,373 lb). Specific impulse: 311 s. Height: 2.83 m (9.28 ft). Diameter: 4.21 m (13.81 ft).

Spacecraft delta v: 2,470 m/s (8,100 ft/sec). Electric System: 33.00 kWh. Battery: 1,600.00 Ah.

Family: Manned spacecraft module. Country: USA. Spacecraft: Apollo LM. Propellants: N2O4/Aerozine-50.

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