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N1U 1965 - B
Part of N1 Block B Family
LOx/Kerosene propellant rocket stage. As per N1 improvement study, 1965. Primarily improved reliability and produceability compared to first model.

Status: Study 1965. Thrust: 13,700.00 kN (3,079,800 lbf). Gross mass: 506,000 kg (1,115,000 lb). Unfuelled mass: 50,000 kg (110,000 lb). Specific impulse: 346 s. Burn time: 110 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: N-IUV-III, N-IU. Propellants: Lox/Kerosene.

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