11D51F

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11D51F

Part of NK-15

Kuznetsov LOx/Kerosene rocket engine. N1F 1965 - A. Study 1965. As described in N1 improvement study, 1965. Block A engine thrust increased.

Status: Study 1965. Date: 1965. Thrust: 1,918.00 kN (431,183 lbf). Specific impulse: 331 s. Specific impulse sea level: 296 s.

Country: Russia. Launch Vehicles: N-IF 1965, N-IFV-III, N-IFV-II-III. Propellants: Lox/Kerosene. Stages: N1F 1965 - A. Agency: Kuznetsov bureau. Bibliography: 275, 283, 306, 319, 341.

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