Gemini LSRS LM

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Gemini LSRS LM

Part of Gemini

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

AKA: Landing Module. Status: Study 1966. Thrust: 88.06 kN (19,797 lbf). Gross mass: 20,000 kg (44,000 lb). Unfuelled mass: 3,300 kg (7,200 lb). Specific impulse: 311 s. Height: 1.80 m (5.90 ft). Diameter: 4.21 m (13.81 ft).

Spacecraft delta v: 2,400 m/s (7,800 ft/sec).

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

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