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Molniya 8K78-0
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 | R-7 aft end
Credit - © Mark Wade
| Gross Mass: 43,400 kg (95,600 lb). Empty Mass: 3,800 kg (8,300 lb). Thrust (vac): 995.300 kN (223,752 lbf). Isp: 314 sec. Burn time: 119 sec. Propellants: Lox/Kerosene. Isp(sl): 257 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-107-8D74K. Cost $ : 5.000 million. First Flight: 1960. Last Flight: 1965. No Launched: 104. No Failed: 1. Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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