| Angara Stage 2 |
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Model: Angara Stage 2. Gross Mass: 75,000 kg (165,000 lb). Empty Mass: 9,000 kg (19,800 lb). Thrust (vac): 1,960.000 kN (440,620 lbf). Isp: 455 sec. Burn time: 225 sec. Propellants: Lox/LH2. Isp(sl): 352 sec. Diameter: 3.90 m (12.70 ft). Span: 12.00 m (39.00 ft). Length: 16.00 m (52.00 ft). Country: Russia. No Engines: 1. Motor: RD-0120M. Status: Development 2004. First Flight: 2000. Unique configuration with oxidizer in core and fuel in two tanks strapped on in parallel - all of rail-transportable 3.9 m diameter. Buildt by NPO Energia to Khrunichev design (their own design for Angara and Energia-M were rejected in favor of Khrunichev version). Masses estimated based on engine selected and vehicle performance. Assumed that engine is throttled back to maintain constant 3-G acceleration. 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 - 2008 except where otherwise noted. |