RD-852
Engine · Ukraine
Original archive entry. The text, images and links below are kept as they were written.
Yuzhnoye Nitric acid/UDMH rocket engine. R-16 (SS-7) stage 2 attitude control engine. Out of Production. Four thrusters are each gimbaled in one single axis.
Chambers: 4. Engine: 133 kg (293 lb). Chamber Pressure: 66.20 bar. Propellant Formulation: AK27/UDMH. Thrust to Weight Ratio: 36.99. Oxidizer to Fuel Ratio: 2.4.
Related
- Family
- Storable liquid
- Country
- Ukraine
- Launch Vehicles
- R-16
- Propellants
- Nitric acid/UDMH
- Agency
- Yuzhnoye
- Bibliography
- 348