RD-217
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Glushko Nitric acid/UDMH rocket engine. R-16 stage 1. Out of Production. Original intended use unknown. Three RD-217 clustered to make RD-218. First flight 1961.
Chambers: 2. Engine: 980 kg (2,160 lb). Chamber Pressure: 73.60 bar. Area Ratio: 18.8. Propellant Formulation: AK27I/UDMH. Thrust to Weight Ratio: 90. Oxidizer to Fuel Ratio: 2.5.
Related
- Family
- Storable liquid
- Country
- Russia
- Propellants
- Nitric acid/UDMH
- Stages
- R-16-1
- Agency
- Glushko bureau
- Bibliography
- 320