Gemini LORV SM

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Gemini LORV SM

Part of Gemini

American manned spacecraft module. Study 1967. Calculated mass based on mission requirements, drawing of spacecraft, dimensions of propellant tanks.

AKA: Service Module. Status: Study 1967. Thrust: 44.03 kN (9,898 lbf). Gross mass: 12,500 kg (27,500 lb). Unfuelled mass: 2,500 kg (5,500 lb). Specific impulse: 311 s. Height: 3.40 m (11.10 ft). Diameter: 5.90 m (19.30 ft).

RCS Coarse No x Thrust: 16 x 440 N. Spacecraft delta v: 1,000 m/s (3,200 ft/sec).

Family: Manned spacecraft module. Country: USA. Spacecraft: Gemini LORV. Propellants: N2O4/UDMH.

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