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LLV L-II
American manned spacecraft module. Study 1966. Landing stage for delivery of up to 13,400 kg payload from lunar orbit to lunar surface. Propulsion 2 x RL10-A3 with N2O4/MMH thrusters for orientation, midcourse, and ullage. Delivery of lunar base elements from lunar orbit to lunar surface.

AKA: L-II. Status: Study 1966. Thrust: 131.21 kN (29,497 lbf). Gross mass: 18,500 kg (40,700 lb). Unfuelled mass: 4,200 kg (9,200 lb). Specific impulse: 444 s. Height: 5.20 m (17.00 ft). Diameter: 6.70 m (21.90 ft).

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



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

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