Vostok 8K72-0 R-7 aft end Credit - © Mark Wade Gross Mass: 43,300 kg (95,400 lb). Empty Mass: 3,710 kg (8,170 lb). Thrust (vac): 970.000 kN (218,060 lbf). Isp: 312 sec. Burn time: 120 sec. Propellants: Lox/Kerosene. Isp(sl): 254 sec. Diameter: 2.68 m (8.79 ft). Span: 2.68 m (8.79 ft). Length: 19.00 m (62.00 ft). Country: Russia. No Engines: 1. Engine: RD-107-8D74. Status: Out of production. Cost $ : 5.000 million. First Flight: 1960. Last Flight: 1960. No Launched: 16. No Failed: 1. Used on Launch Vehicles: Vostok 8K72.                   Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2007 except where otherwise noted.

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