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Luna 8K72-2
Part of Block L Family
LOx/Kerosene propellant rocket stage. .

Status: Retired 1960. Thrust: 49.00 kN (11,015 lbf). Gross mass: 8,100 kg (17,800 lb). Unfuelled mass: 1,120 kg (2,460 lb). Specific impulse: 316 s. Burn time: 440 s. Height: 2.84 m (9.31 ft). Diameter: 2.56 m (8.39 ft). Span: 2.56 m (8.39 ft).

Cost $ : 3.000 million.



Country: Russia. Engines: RD-0105. Launch Vehicles: Vostok-L 8K72. Propellants: Lox/Kerosene.

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