This page no longer updated from 31 October 2001. Latest version can be found at NK-15VM

Manufacturer Name: NK-15VM. Government Designation: 11D52VM. Other Designations: NK-35. Designer: Kuznetsov. Developed in: 1965. Application: N-1 stage 2 (block B) replacement. Used on stages: N1 Block V-II. Used on launch vehicles: N-IFV-II, III, N-IMV-II, III. Propellants: Lox/LH2 Thrust(vac): 200,000 kgf. Thrust(vac): 1,960.00 kN. Chambers: 1. Country: Russia. Status: Developed 1965. References: 283 . Comments: 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.
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Last update 12 March 2001.
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© Mark Wade, 2001 .