RO-31
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Kosberg nuclear/LH2 rocket engine. UR-700 Third Stage. Study 1967. Engine proposed for UR-700 third stage to achieve 250 metric ton payload to low earth orbit. Probably closely related to RD-0411.
Propellant Formulation: Nuclear/LH2/Methane.
Related
- Family
- nuclear-powered
- Country
- Russia
- Launch Vehicles
- UR-700 / RO-31
- Propellants
- Nuclear/LH2
- Stages
- UR-700-RO-31
- Agency
- Kosberg bureau
- Bibliography
- 443