N1U 1965

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N1U 1965 - V

Part of N1 Block V

LOx/Kerosene propellant rocket stage. As per N1 improvement study, 1965. Primarily improved reliability and produceability compared to first model.

Status: Study 1965. Thrust: 1,560.00 kN (350,700 lbf). Gross mass: 193,000 kg (425,000 lb). Unfuelled mass: 15,000 kg (33,000 lb). Specific impulse: 347 s. Burn time: 380 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: N-IU. Propellants: Lox/Kerosene.

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