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Soyuz M-1
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Gross Mass: 100,500 kg (221,500 lb). Empty Mass: 6,000 kg (13,200 lb). Thrust (vac): 872.000 kN (196,033 lbf). Isp: 336 sec. Burn time: 310 sec. Propellants: Lox/Kerosene. Isp(sl): 298 sec. Diameter: 2.95 m (9.67 ft). Span: 2.95 m (9.67 ft). Length: 28.00 m (91.00 ft). Country: Russia. No Engines: 1. Engine: RD-120K. Status: Development ended 2000. Last Flight: 0. No Launched: 0. No Failed: 0.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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