11D52M
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Kuznetsov LOx/Kerosene rocket engine. N1M 1965 - B. Study 1965. As per N1 improvement study, 1965. Thrust increased to 280 metric tons per engine.
Related
- Country
- Russia
- Propellants
- Lox/Kerosene
- Stages
- N1M 1965 - B
- Agency
- Kuznetsov bureau