N1U 1965 - A (original) (raw)

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N1U 1965 - A

Part of N1 Block A

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

Status: Study 1965. Thrust: 49,420.00 kN (11,110,050 lbf). Gross mass: 1,934,000 kg (4,263,000 lb). Unfuelled mass: 195,000 kg (429,000 lb). Specific impulse: 331 s. Specific impulse sea level: 296 s. Burn time: 110 s. Height: 30.00 m (98.00 ft). Diameter: 10.00 m (32.00 ft). Span: 17.00 m (55.00 ft).

No Engines: 30.

Country: Russia. Engines: NK-15. Launch Vehicles: N-IUV-III, N-IU. Propellants: Lox/Kerosene.

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