Encyclopedia Astronautica Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9 A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z NK-15VM 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. Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9 A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z � 1997-2016 Mark Wade - Contact � / Conditions for Use |
