11D53M

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11D53M

Part of NK-9

Kuznetsov LOx/Kerosene rocket engine. N1M 1965 - V. Study 1965. As per N1 improvement study, 1965. Further increase in thrust of Block V engines. Used on N-IM 1965 launch vehicle.

Status: Study 1965. Date: 1965. Thrust: 735.00 kN (165,234 lbf). Specific impulse: 347 s.

Country: Russia. Launch Vehicles: N-IM 1965. Propellants: Lox/Kerosene. Stages: N1M 1965 - V. Agency: Kuznetsov bureau.

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