RD-0211
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Kosberg N2O4/UDMH rocket engine. Proton stage 2. Out of Production. Variant of RD-0210 providing tank pressurization. Staged combustion cycle.
Thrust (sl): 421.900 kN (94,847 lbf). Thrust (sl): 43,020 kgf. Engine: 566 kg (1,247 lb). Chamber Pressure: 147.00 bar. Area Ratio: 81.3. Thrust to Weight Ratio: 104.87.
Related
- Family
- Storable liquid
- Country
- Russia
- Propellants
- N2O4/UDMH
- Stages
- Proton K-2
- Agency
- Kosberg bureau