Molniya 8K78M-1 R-7 aft end Credit - © Mark Wade Gross Mass: 100,600 kg (221,700 lb). Empty Mass: 6,798 kg (14,987 lb). Thrust (vac): 976.700 kN (219,571 lbf). Isp: 315 sec. Burn time: 291 sec. Propellants: Lox/Kerosene. Isp(sl): 248 sec. Diameter: 2.99 m (9.80 ft). Span: 2.60 m (8.50 ft). Length: 28.00 m (91.00 ft). Country: Russia. No Engines: 1. Engine: RD-108-8D727. Cost $ : 13.000 million. First Flight: 1964. Last Flight: 2006. No Launched: 294. 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.

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