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N1 1962 - V
Part of N1 Block V Family
LOx/Kerosene propellant rocket stage. Compared to total fuelled mass excludes 1,000 kg in propellants lost to boil-off prior to stage ignition. Values as in draft project as defended on 2-16 July 1962.

Status: Study 1962. Thrust: 1,560.00 kN (350,700 lbf). Gross mass: 193,000 kg (425,000 lb). Unfuelled mass: 16,000 kg (35,000 lb). Specific impulse: 347 s. Burn time: 368 s. Height: 12.00 m (39.00 ft). Diameter: 4.80 m (15.70 ft). Span: 6.80 m (22.30 ft).

No Engines: 4.

Country: Russia. Engines: NK-19. Launch Vehicles: N1 1962. Propellants: Lox/Kerosene.



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