RD-210
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Glushko Nitric acid/Kerosene rocket engine. vertical sounding rocket. Developed -1954.
Engine: 81 kg (178 lb). Chamber Pressure: 23.50 bar. Area Ratio: 4.16. Propellant Formulation: HNO3/TM-114. Thrust to Weight Ratio: 37.76. Oxidizer to Fuel Ratio: 4.12.
Related
- Family
- Storable liquid
- Country
- Russia
- Propellants
- Nitric acid/Kerosene
- Agency
- Glushko bureau
- Bibliography
- 320