N1 1964 - B
Stage · Russia
Original archive entry. The text, images and links below are kept as they were written.
LOx/Kerosene propellant rocket stage. Second stage of the N1 superbooster. As per draft project for N1-L3, 1964. Specific impulse estimate down one second from 1962 draft project. Thrust said to be increased 2% but not reflected in figures given.
No Engines: 8.
Related
- Country
- Russia
- Engines
- NK-15V
- Launch Vehicles
- N1 1964
- Propellants
- Lox/Kerosene