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Buran M-41
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Gross Mass: 18,000 kg (39,000 lb). Empty Mass: 3,000 kg (6,600 lb). Thrust (vac): 755.000 kN (169,730 lbf). Isp: 254 sec. Burn time: 50 sec. Propellants: Nitric acid/Kerosene. Isp(sl): 231 sec. Diameter: 1.20 m (3.90 ft). Span: 3.00 m (9.80 ft). Length: 19.10 m (62.60 ft). Country: Russia. No Engines: 1. Engine: RD-213. Status: Development ended 1957. Booster for Buran missile. Four used to boost ramjet second stage to ignition conditions. Masses estimated based on missile known total mass. Specific impulse estimated.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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