GR-1 Stage 3
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. This stage was a close cousin of that developed for the Molniya launch vehicle.
Related
- Country
- Russia
- Engines
- 8D726
- Launch Vehicles
- 8K513
- Propellants
- Lox/Kerosene