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LLV L-I
American manned spacecraft module. Study 1966. Lunar Orbit Insertion stage for placing LLV into lunar orbit. Propulsion 2 x RL10-A3 with N2O4/MMH thrusters for orientation, midcourse, and ullage. Lunar orbit insertion of Lunar Logistics Vehicle lander and payload.

AKA: L-I. Status: Study 1966. Thrust: 131.21 kN (29,497 lbf). Gross mass: 10,500 kg (23,100 lb). Unfuelled mass: 1,300 kg (2,800 lb). Specific impulse: 444 s. Height: 2.70 m (8.80 ft). Diameter: 6.70 m (21.90 ft).

Spacecraft delta v: 1,100 m/s (3,600 ft/sec).



Family: Manned spacecraft module. Country: USA. Spacecraft: LLV. Propellants: Lox/LH2.

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