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N-11 1963 - V
Part of N1 Block G Family
LOx/Kerosene propellant rocket stage. Conjectural stage derived from GR-1 stage 1 to match total mass given of launch vehicle.

Status: Study 1963. Thrust: 784.00 kN (176,250 lbf). Gross mass: 70,000 kg (154,000 lb). Unfuelled mass: 6,000 kg (13,200 lb). Specific impulse: 347 s. Burn time: 273 s. Height: 18.00 m (59.00 ft). Diameter: 2.68 m (8.79 ft). Span: 2.68 m (8.79 ft).

No Engines: 4.



Country: Russia. Engines: NK-19. Launch Vehicles: N11 1963. Propellants: Lox/Kerosene.

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