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N-11 1963 - V
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Gross Mass: 70,000 kg (154,000 lb). Empty Mass: 6,000 kg (13,200 lb). Thrust (vac): 784.000 kN (176,250 lbf). Isp: 347 sec. Burn time: 273 sec. Propellants: Lox/Kerosene. Diameter: 2.68 m (8.79 ft). Span: 2.68 m (8.79 ft). Length: 18.00 m (59.00 ft). Country: Russia. No Engines: 4. Engine: NK-19. Status: Study 1963. Conjectural stage derived from GR-1 stage 1 to match total mass given of launch vehicle.
Used on Launch Vehicles:
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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