RD-0221
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
CADB Museum, March 1992.
Credit: © Dietrich Haeseler
Kosberg N2O4/UDMH rocket engine. upper stage of unnamed missile by Mishin. Developed 1965-70.
Chambers: 1 + 2. Engine: 150 kg (330 lb). Chamber Pressure: 122.60 bar. Thrust to Weight Ratio: 53.02.
Related
- Family
- Storable liquid
- Country
- Russia
- Propellants
- N2O4/UDMH
- Agency
- Kosberg bureau
- Bibliography
- 307