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Soyuz 11A511U-1
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 | R-7 aft end
Credit - © Mark Wade
| Gross Mass: 105,400 kg (232,300 lb). Empty Mass: 6,875 kg (15,156 lb). Thrust (vac): 997.091 kN (224,155 lbf). Isp: 311 sec. Burn time: 286 sec. Propellants: Lox/Kerosene. Isp(sl): 245 sec. Diameter: 2.95 m (9.67 ft). Span: 2.95 m (9.67 ft). Length: 27.80 m (91.20 ft). Country: Russia. No Engines: 1. Engine: RD-108-11D512. Status: Design 2000. Cost $ : 13.000 million. First Flight: 1973. Last Flight: 2006. No Launched: 720. No Failed: 2. Gross mass includes 2600 kg of hydrogen peroxide and 520 kg of liquid nitrogen expended during ascent but not contributing to propulsion. Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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