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Angara UM
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Gross Mass: 140,000 kg (300,000 lb). Empty Mass: 10,000 kg (22,000 lb). Thrust (vac): 2,094.700 kN (470,907 lbf). Isp: 338 sec. Burn time: 300 sec. Propellants: Lox/Kerosene. Isp(sl): 310 sec. Diameter: 2.90 m (9.50 ft). Span: 2.90 m (9.50 ft). Length: 25.00 m (82.00 ft). Country: Russia. No Engines: 1. Engine: RD-191. Status: In development. Can be throttled to 95%. Propellant ration 2.6:1, chamber pressure 257 bar.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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