11D52M

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11D52M

Part of NK-15

Kuznetsov LOx/Kerosene rocket engine. N1M 1965 - B. Study 1965. As per N1 improvement study, 1965. Thrust increased to 280 metric tons per engine.

Status: Study 1965. Date: 1965. Thrust: 2,745.00 kN (617,100 lbf). Specific impulse: 330 s. Specific impulse sea level: 296 s.

Country: Russia. Launch Vehicles: N-IM 1965, N-IMV-III. Propellants: Lox/Kerosene. Stages: N1M 1965 - B. Agency: Kuznetsov bureau.

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