8K513 Blok B
Stage · Russia
Original archive entry. The text, images and links below are kept as they were written.
LOx/Kerosene propellant rocket stage. Masses estimated based on total vehicle mass of 117 metric tons. Developed into Molniya/Soyuz second stage.
Related
- Country
- Russia
- Engines
- NK-9V
- Launch Vehicles
- 8K513
- Propellants
- Lox/Kerosene