RD-274
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Glushko N2O4/UDMH rocket engine. Developed 1975-85. Upgrade of RD-264 engine with increased chamber pressure and thrust. Development stopped due to problems with turbopump shaft balance.
Other sources say development was completed and the engine was built for the R-36M2 ICBM. Consists of four RD-273 engines.
Chambers: 4. Chamber Pressure: 226.00 bar.
Related
- Family
- Storable liquid
- Country
- Russia
- Launch Vehicles
- R-36M2 15A18M, Dnepr
- Propellants
- N2O4/UDMH
- Agency
- Glushko bureau