NK-15VM

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NK-15VM

Part of NK-15

Kuznetsov LOx/LH2 rocket engine. N-1 stage 2 (block B) replacement. Design 1972. Derivative of NK-15 with kerosene replaced by hydrogen. Canceled before hot-tests.

AKA: 11D52VM;NK-35. Status: Design 1972. Date: 1965. Thrust: 1,960.00 kN (440,620 lbf).

Derivative of NK-15 with kerosene replaced by hydrogen. Canceled before hot-tests. Intended for cryogenic second stage of N-IFV-II,III or N-IMV-II,III launcher versions studied in 1965.

Country: Russia. Launch Vehicles: N-IFV-II-III, N-IMV-II-III. Propellants: Lox/LH2. Stages: UR-700M-3, N1 Block V-II. Agency: Kuznetsov bureau.

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