RD-853
Engine · Ukraine
Original archive entry. The text, images and links below are kept as they were written.
Credit: via Dietrich Haeseler
Yuzhnoye Nitric acid/UDMH rocket engine. Stage 2, no application. Developed 1960-63. Designed for second stage, no application. Two thrust levels. Thrust 467.6 kN + 11.8 kN / 7.65 kN.
Chambers: 1 + 4. Engine: 485 kg (1,069 lb). Chamber Pressure: 83.60 bar. Propellant Formulation: AK27/UDMH. Thrust to Weight Ratio: 98.31. Oxidizer to Fuel Ratio: 2.41.
Related
- Family
- Storable liquid
- Country
- Ukraine
- Propellants
- Nitric acid/UDMH
- Agency
- Yuzhnoye
- Bibliography
- 348