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Luna 8K72-0
Part of R-7 Block BVGD stage series Family
LOx/Kerosene propellant rocket stage. .

Status: Retired 1960. Thrust: 990.00 kN (222,560 lbf). Gross mass: 43,400 kg (95,600 lb). Unfuelled mass: 3,800 kg (8,300 lb). Specific impulse: 312 s. Specific impulse sea level: 254 s. Burn time: 120 s. Height: 19.00 m (62.00 ft). Diameter: 2.68 m (8.79 ft). Span: 2.68 m (8.79 ft).

Cost $ : 5.000 million.



Country: Russia. Engines: RD-107-8D74-1958. Launch Vehicles: Sputnik 8K71PS, Vostok-L 8K72. Propellants: Lox/Kerosene.

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