RD-280
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Glushko N2O4/Aerozine-50 rocket engine. Experimental engine. Study 1961. Experimental engine using Aerozine 50 (50% UDMH + 50% hydrazine) as fuel.
Engine: 174 kg (383 lb). Chamber Pressure: 147.00 bar. Thrust to Weight Ratio: 68.91. Oxidizer to Fuel Ratio: 1.718.
Subtopics
- 8D725 Glushko N2O4/UDMH rocket engine. Developed 1963-1970. 10 to 12 metric ton thrust engine developed for an unstated military requirement.
Related
- Family
- Storable liquid
- Country
- Russia
- Propellants
- N2O4/Aerozine-50
- Stages
- R-56 Block K
- Agency
- Glushko bureau
- Bibliography
- 317