RD-224
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 1. Out of production. RD-224 is a block of 2 RD-225s. An upper stage thrust chamber was developed under designation U102-000. First flight 1961.
Chambers: 4. Engine: 1,250 kg (2,750 lb). Chamber Pressure: 83.40 bar. Area Ratio: 21. Propellant Formulation: AK27P/UDMH. Thrust to Weight Ratio: 145.04. Oxidizer to Fuel Ratio: 2.5.
Related
- Family
- Storable liquid
- Country
- Russia
- Launch Vehicles
- R-26
- Propellants
- Nitric acid/UDMH
- Stages
- R-26-1
- Agency
- Glushko bureau
- Bibliography
- 320