N1M 1965 - B
Stage · Russia
Original archive entry. The text, images and links below are kept as they were written.
LOx/Kerosene propellant rocket stage. As per N1 improvement study, 1965. Further stretch of Block B and thrust increased again to 280 metric tons per engine.
No Engines: 8.
Related
- Country
- Russia
- Engines
- 11D52M
- Propellants
- Lox/Kerosene