RD-222
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Glushko Nitric acid/UDMH rocket engine. missile stage 1 (stage 2 used RD-223). Developed 1960-61. Precursor to RD-253.
Engine: 980 kg (2,160 lb). Chamber Pressure: 147.00 bar. Area Ratio: 26.3. Propellant Formulation: AK27P/UDMH. Thrust to Weight Ratio: 170.02. Oxidizer to Fuel Ratio: 2.92.
Related
- Family
- Storable liquid
- Country
- Russia
- Propellants
- Nitric acid/UDMH
- Agency
- Glushko bureau
- Bibliography
- 320