11D51M
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Kuznetsov LOx/Kerosene rocket engine. N1M 1965 - A. Study 1965. As described in N1 improvement study, 1965. Huge modification of Block A engines - sea level thrust increased from 175 metric tons thrust to 250 metric tons.
Related
- Country
- Russia
- Launch Vehicles
- N-IM 1965, N-IMV-III, N-IMV-II-III
- Propellants
- Lox/Kerosene
- Stages
- N1M 1965 - A
- Agency
- Kuznetsov bureau