U102-000
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Glushko Nitric acid/UDMH rocket engine. R-26 stage 2. Out of production.
Orevo has sectioned hardware. This is only the thrust chamber, probably based on RD-224 chamber. Other components like turbopumps, etc. were obviously the same as RD-224. Mass chamber only 198 kg.
Chamber Pressure: 83.60 bar. Area Ratio: 48.4. Propellant Formulation: AK27P/UDMH. Oxidizer to Fuel Ratio: 2.76.
Related
- Family
- Storable liquid
- Country
- Russia
- Launch Vehicles
- R-26
- Propellants
- Nitric acid/UDMH
- Stages
- R-26-2
- Agency
- Glushko bureau