YF-23

Engine · China

Original archive entry. The text, images and links below are kept as they were written.

Beijing Wan Yuan N2O4/UDMH rocket engine. In Production. Used as vernier motor with YF-22 and YF-25.

Thrust (sl): 10.200 kN (2,293 lbf). Thrust (sl): 1,036 kgf. Thrust to Weight Ratio: 0.

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