RD-220
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-221). Developed 1960-.
Engine: 760 kg (1,670 lb). Chamber Pressure: 147.00 bar. Area Ratio: 31.8. Propellant Formulation: AK27P/UDMH. Thrust to Weight Ratio: 144.1. Oxidizer to Fuel Ratio: 2.8.
Subtopics
- RD-221 Glushko Nitric acid/UDMH rocket engine. missile stage 2 (stage 1 used RD-220). Developed 1960-.
Related
- Family
- Storable liquid
- Country
- Russia
- Propellants
- Nitric acid/UDMH
- Agency
- Glushko bureau
- Bibliography
- 320