Gemini LSRS LOIM

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Gemini LSRS LOIM

Part of Gemini

American manned spacecraft module. Study 1966. Calculated mass based on mission requirements, drawing of spacecraft, dimensions of propellant tanks.

AKA: Lunar Orbit Insertion Module. Status: Study 1966. Thrust: 62.27 kN (13,999 lbf). Gross mass: 8,000 kg (17,600 lb). Unfuelled mass: 800 kg (1,760 lb). Specific impulse: 311 s. Height: 3.45 m (11.31 ft). Diameter: 4.21 m (13.81 ft).

Spacecraft delta v: 3,200 m/s (10,400 ft/sec).

Family: Manned spacecraft module. Country: USA. Spacecraft: Gemini Lunar Surface Rescue Spacecraft. Propellants: N2O4/UDMH.

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