N-111-A

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N-111-A

Part of N1 Block V

LOx/Kerosene propellant rocket stage. Variant of N1 Block V for first stage use. Number of engines would have to be increased and reduced expansion ratio nozzles fitted for sea level use. Least attractive of N1 variants and seems not to have been pursued after draft project.

Status: Study 1962. Thrust: 2,540.00 kN (571,010 lbf). Gross mass: 192,000 kg (423,000 lb). Unfuelled mass: 20,000 kg (44,000 lb). Specific impulse: 331 s. Specific impulse sea level: 296 s. Burn time: 216 s. Height: 12.00 m (39.00 ft). Diameter: 4.80 m (15.70 ft). Span: 6.80 m (22.30 ft).

No Engines: 12.

Country: Russia. Engines: NK-19. Launch Vehicles: N111. Propellants: Lox/Kerosene.

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