RD-0213
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Kosberg N2O4/UDMH rocket engine. Proton stage 3. Design 1962. Version of RD-0210. Staged combustion cycle (Oxidizer pre-burner gas routed to main chamber after driving turbine). Main engine for Proton Stage 3 in system RD-0212.
Chambers: 4. Thrust (sl): 446.000 kN (100,264 lbf). Thrust (sl): 45,476 kgf. Chamber Pressure: 147.00 bar. Area Ratio: 81.3.
Related
- Family
- Storable liquid
- Country
- Russia
- Launch Vehicles
- Monoblock UR-500, Polyblock UR-500
- Propellants
- N2O4/UDMH
- Stages
- R-56 Block O, Monoblock UR-500-2
- Agency
- Kosberg bureau