Soyuz M-0 Gross Mass: 42,200 kg (93,000 lb). Empty Mass: 3,000 kg (6,600 lb). Thrust (vac): 872.000 kN (196,033 lbf). Isp: 336 sec. Burn time: 145 sec. Propellants: Lox/Kerosene. Isp(sl): 298 sec. Diameter: 2.68 m (8.79 ft). Span: 2.68 m (8.79 ft). Length: 20.00 m (65.00 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: 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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