RD-0231
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Kosberg N2O4/UDMH rocket engine. P-700 Granit. Out of Production. Staged combustion cycle. First flight 1970.
Engine: 28 kg (61 lb). Chamber Pressure: 123.00 bar. Thrust to Weight Ratio: 105.71.
Related
- Family
- Storable liquid
- Country
- Russia
- Spacecraft
- Granat
- Propellants
- N2O4/UDMH
- Agency
- Kosberg bureau
- Bibliography
- 307