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Soyuz M-3
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Gross Mass: 5,000 kg (11,000 lb). Empty Mass: 1,000 kg (2,200 lb). Thrust (vac): 20.000 kN (4,496 lbf). Isp: 360 sec. Burn time: 700 sec. Propellants: Lox/Kerosene. Isp(sl): 0 sec. Diameter: 2.40 m (7.80 ft). Span: 2.40 m (7.80 ft). Length: 2.70 m (8.80 ft). Country: Russia. No Engines: 1. Engine: RD-161-1. Status: Development ended 2000. Last Flight: 0. No Launched: 0. No Failed: 0. Empty mass estimated. Multiple restart engine.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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