Soyuz 11A511U-2 RD-0110 Engine Soyuz 11A511 Stage 2 engine displayed at Tsiolkovskiy Museum in Kaluga. Credit - © Mark Wade Gross Mass: 25,200 kg (55,500 lb). Empty Mass: 2,355 kg (5,191 lb). Thrust (vac): 298.100 kN (67,016 lbf). Isp: 330 sec. Burn time: 250 sec. Propellants: Lox/Kerosene. Diameter: 2.66 m (8.72 ft). Span: 2.66 m (8.72 ft). Length: 6.74 m (22.11 ft). Country: Russia. No Engines: 1. Engine: RD-0110. Status: Design 2000. Cost $ : 3.000 million. First Flight: 1973. Last Flight: 2006. No Launched: 720. No Failed: 3. Used on Launch Vehicles: Soyuz 11A511U. Soyuz 11A511U / Fregat. Soyuz 11A511U / Ikar. Soyuz M.                   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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