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N-11 Block B
Part of N1 Block V Family
LOx/Kerosene propellant rocket stage. Derived from N1 Block V.

Status: Study 1963. Thrust: 1,560.00 kN (350,700 lbf). Gross mass: 192,000 kg (423,000 lb). Unfuelled mass: 18,000 kg (39,000 lb). Specific impulse: 347 s. Burn time: 372 s. Height: 12.00 m (39.00 ft). Diameter: 4.80 m (15.70 ft). Span: 6.80 m (22.30 ft).

No Engines: 8.



Country: Russia. Engines: NK-19. Launch Vehicles: N11GR, N11 1963. Propellants: Lox/Kerosene.

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