Molniya 8K78M-2 RD-0110 Engine Soyuz 11A511 Stage 2 engine displayed at Tsiolkovskiy Museum in Kaluga. Credit - © Mark Wade Gross Mass: 24,800 kg (54,600 lb). Empty Mass: 1,976 kg (4,356 lb). Thrust (vac): 298.100 kN (67,016 lbf). Isp: 330 sec. Burn time: 241 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-0110. Cost $ : 3.000 million. First Flight: 1964. Last Flight: 2006. No Launched: 294. No Failed: 1. Used on Launch Vehicles: Molniya 8K78M.                   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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