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N1F Block B
Part of N1 Block B Family
LOx/Kerosene propellant rocket stage. Includes 3,500 kg for Stage 2-3 interstage.

Status: Development ended 1974. Thrust: 14,040.00 kN (3,156,318 lbf). Gross mass: 620,000 kg (1,360,000 lb). Unfuelled mass: 55,700 kg (122,700 lb). Specific impulse: 346 s. Burn time: 120 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-43. Launch Vehicles: N1F, N1F Sr, N1F-L3M. Propellants: Lox/Kerosene.

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