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N1 1964 - V
Part of N1 Block V Family
LOx/Kerosene propellant rocket stage. As per draft project for N1-L3, 1964. Thrust said to be increased 2% but not reflected in figures given.

Status: Development ended 1964. 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 1964. Propellants: Lox/Kerosene.



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