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NK-35
Part of NK-15 Family
Kuznetsov LOx/LH2 rocket engine. Design 1972. Derivative of the NK-15 with kerosene replaced by hydrogen. The engine was canceled before hot-tests. Proposed for the UR-700M Mars booster in 1972, but this was not approved either.

Status: Design 1972. Date: 1972. Thrust: 1,960.00 kN (440,620 lbf).

The NK-15VM was a derivative of the NK-15 with kerosene replaced by hydrogen. The engine was canceled before hot-tests. The design was updated and proposed for the UR-700M Mars booster in 1972, but this was not approved either.



Country: Russia. Launch Vehicles: UR-700M. Propellants: Lox/LH2. Stages: UR-700M-3. Agency: Kuznetsov bureau. Bibliography: 443.

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