NK-9V
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Kuznetsov LOx/Kerosene rocket engine. N-1 stage 2 / N-1 stage 3 / R-9 Stage 2. Developed for 2nd stage of the R-9 ICBM (alternative to RD-111 engine by OKB-456). NK-9 with increased expansion ratio. First flight 1965.
Thrust (sl): 360.390 kN (81,019 lbf). Thrust (sl): 36,750 kgf. Propellant Formulation: Lox/RG-1.
Related
- Country
- Russia
- Launch Vehicles
- R-9A
- Propellants
- Lox/Kerosene
- Stages
- 8K513 Blok B
- Agency
- Kuznetsov bureau