11D51M

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11D51M

Part of NK-15

Kuznetsov LOx/Kerosene rocket engine. N1M 1965 - A. Study 1965. As described in N1 improvement study, 1965. Huge modification of Block A engines - sea level thrust increased from 175 metric tons thrust to 250 metric tons.

Status: Study 1965. Date: 1965. Thrust: 2,843.00 kN (639,131 lbf). Specific impulse: 346 s.

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

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