N1M 1965 - A
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. Huge modification of Block A, almost double propellant capacity, engines increased from 175 metric tons thrust to 250 metric tons.
No Engines: 30.
Related
- Country
- Russia
- Engines
- 11D51M
- Launch Vehicles
- N-IM 1965, N-IMV-III, N-IMV-II-III
- Propellants
- Lox/Kerosene