YF-75
Engine · China
Original archive entry. The text, images and links below are kept as they were written.
Beijing Wan Yuan LOx/LH2 rocket engine. In development. Gas-generator turbopump. Gimbaled engine. First flight 1994.
Chamber Pressure: 37.60 bar. Area Ratio: 80. Thrust to Weight Ratio: 0. Oxidizer to Fuel Ratio: 5. Restarts: 2.
Related
- Country
- China
- Spacecraft
- CZ H-18
- Launch Vehicles
- Chang Zheng 3A, Chang Zheng 3B, CZ-NGLV-320, CZ-NGLV-522/HO, Chang Zheng 3C, CZ-NGLV-504/HO, CZ-NGLV-540/HO
- Propellants
- Lox/LH2
- Stages
- CZ H-18 stage, CZ-NGLV-HO
- Agency
- Beijing Wan Yuan