11D52F

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11D52F

Part of NK-15

Kuznetsov LOx/Kerosene rocket engine. N1F 1965 - B. Study 1965. As per N1 improvement study, 1965. Engine thrust increased from 150 t each to 200 t.

Status: Study 1965. Date: 1965. Thrust: 1,961.00 kN (440,850 lbf). Specific impulse: 347 s.

Country: Russia. Launch Vehicles: N-IF 1965, N-IFV-III. Propellants: Lox/Kerosene. Stages: N1F 1965 - B. Agency: Kuznetsov bureau.

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