RD-172
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Glushko LOx/Kerosene rocket engine. Zenit-3 stage 1 (?). Developed -1994. Uprated version of RD-171. To have been qualified for flight 1994.
Chambers: 4. Engine: 11,703 kg (25,800 lb). Chamber Pressure: 258.90 bar. Area Ratio: 36.87. Thrust to Weight Ratio: 72.79. Oxidizer to Fuel Ratio: 2.6.
Related
- Country
- Russia
- Propellants
- Lox/Kerosene
- Agency
- Glushko bureau
- Bibliography
- 354