GR-1 Stage 1
Stage · Russia
Original archive entry. The text, images and links below are kept as they were written.
LOx/Kerosene propellant rocket stage. Payload 4,000 kg (2.2 MT nuclear warhead). Range 13,000 km or orbital. Accuracy (90%) 5 km in range and 3 km in dispersion. Masses estimated based on total vehicle mass of 117 metric tons.
No Engines: 4.
Related
- Country
- Russia
- Engines
- NK-9
- Launch Vehicles
- 8K513
- Propellants
- Lox/Kerosene