Luna 8K72-0 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): 990.000 kN (222,560 lbf). Isp: 312 sec. Burn time: 120 sec. Propellants: Lox/Kerosene. Isp(sl): 254 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-107-8D74-1958. Status: Out of production. Cost $ : 5.000 million. First Flight: 1958. Last Flight: 1960. No Launched: 36. No Failed: 2. Used on Launch Vehicles: Luna 8K72.                   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