RD-211
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Glushko Nitric acid/Kerosene rocket engine. long-distance missile. Developed 1952-55. Original four-chamber engine design planned for use on the R-12 IRBM. Abandoned due to limited thrust and the RD-214 was developed in its place.
Chambers: 4. Engine: 635 kg (1,400 lb). Chamber Pressure: 39.20 bar. Area Ratio: 9.52. Propellant Formulation: AK20/TM-185. Thrust to Weight Ratio: 103.11. Oxidizer to Fuel Ratio: 4.05.
Related
- Family
- Storable liquid
- Country
- Russia
- Propellants
- Nitric acid/Kerosene
- Agency
- Glushko bureau