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Luna 8K72-2
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Gross Mass: 8,100 kg (17,800 lb). Empty Mass: 1,120 kg (2,460 lb). Thrust (vac): 49.000 kN (11,015 lbf). Isp: 316 sec. Burn time: 440 sec. Propellants: Lox/Kerosene. Isp(sl): 0 sec. Diameter: 2.56 m (8.39 ft). Span: 2.56 m (8.39 ft). Length: 2.84 m (9.31 ft). Country: Russia. No Engines: 1. Engine: RD-0105. Status: Out of production. Cost $ : 3.000 million. First Flight: 1958. Last Flight: 1960. No Launched: 9. No Failed: 1.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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