Soyuz 11A511U2-2 RD-0110 Engine Soyuz 11A511 Stage 2 engine displayed at Tsiolkovskiy Museum in Kaluga. Credit - © Mark Wade Gross Mass: 25,400 kg (55,900 lb). Empty Mass: 2,400 kg (5,200 lb). Thrust (vac): 298.100 kN (67,016 lbf). Isp: 330 sec. Burn time: 250 sec. Propellants: Lox/Kerosene. Isp(sl): 0 sec. 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: Out of production. Cost $ : 3.000 million. First Flight: 1982. Last Flight: 1995. No Launched: 92. Used on Launch Vehicles: Soyuz 11A511U2.                   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.

Encyclopedia Astronautica topic index 0 - A - B - C - D - E - F - G - H - I - J - K - L - M - N - O - P - Q - Ra - Re - Sa - Sf - Sp - T - U - V - W - X - Y - Z Enter your search terms   Web www.astronautix.com Submit search form