| UR-700M-3 |
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Model: UR-700M-3. Gross Mass: 2,000,000 kg (4,400,000 lb). Empty Mass: 200,000 kg (440,000 lb). Thrust (vac): 11,700.000 kN (2,630,200 lbf). Isp: 455 sec. Burn time: 670 sec. Propellants: Lox/LH2. Diameter: 12.50 m (41.00 ft). Span: 12.50 m (41.00 ft). Length: 16.00 m (52.00 ft). Country: Russia. No Engines: 6. Motor: NK-15VM. Status: Design 1972. Total mass, length, estimated based on empty mass, total vehicle mass. Engine specific impulse estimated based on performance requirements. Used on Launch Vehicles: 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. |