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N1 1962 - B
Part of N1 Block B Family
LOx/Kerosene propellant rocket stage. Includes 3500 kg Stage 2-Stage 3 interstage. 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: 13,778.00 kN (3,097,417 lbf). Gross mass: 506,000 kg (1,115,000 lb). Unfuelled mass: 50,000 kg (110,000 lb). Specific impulse: 347 s. Burn time: 106 s. Height: 20.00 m (65.00 ft). Diameter: 6.80 m (22.30 ft). Span: 9.80 m (32.10 ft).

No Engines: 8.

Country: Russia. Engines: NK-15V. Launch Vehicles: N1 1962. Propellants: Lox/Kerosene.



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