NK-15VM
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
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.
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.
Related
- 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