RD-161-1
Engine · Russia
Original archive entry. The text, images and links below are kept as they were written.
Glushko LOx/Kerosene rocket engine. Development ended 2000. Proposed for use on Soyuz M-3. Basic version. Engine Cycle: closed gas generator. Feed Method: turbopump.
Engine: 119 kg (262 lb). Chamber Pressure: 117.70 bar. Area Ratio: 351.6. Thrust to Weight Ratio: 16.8. Oxidizer to Fuel Ratio: 2.6.
Related
- Country
- Russia
- Propellants
- Lox/Kerosene
- Stages
- Soyuz M-3
- Agency
- Glushko bureau
- Bibliography
- 318