RD-854
Engine · Ukraine
Original archive entry. The text, images and links below are kept as they were written.
Credit: via Dietrich Haeseler
Yuzhnoye N2O4/UDMH rocket engine. R-36orb (SS-X-10) orbital stage. Out of Production. Thrust vector control by 4 nozzles fed from gas generator.
Chambers: 1 + 4. Engine: 100 kg (220 lb). Chamber Pressure: 85.30 bar. Thrust to Weight Ratio: 76.99. Oxidizer to Fuel Ratio: 2.02.
Related
- Family
- Storable liquid
- Country
- Ukraine
- Launch Vehicles
- R-36O 8K69
- Propellants
- N2O4/UDMH
- Agency
- Yuzhnoye
- Bibliography
- 348