RD-261
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Glushko N2O4/UDMH rocket engine. Tsyklon 3 stage 1. In production. Based on RD-251 First flight 1977.
Chambers: 6. Engine: 1,764 kg (3,888 lb). Chamber Pressure: 83.00 bar. Area Ratio: 14.7. Thrust to Weight Ratio: 175.27. Oxidizer to Fuel Ratio: 2.6.
Related
- Family
- Storable liquid
- Country
- Russia
- Launch Vehicles
- Tsiklon-3
- Propellants
- N2O4/UDMH
- Stages
- Tsyklon 3-1
- Agency
- Glushko bureau