YF-23 (original) (raw)

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YF-23

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

Status: In Production. Thrust: 11.00 kN (2,472 lbf). Specific impulse: 282 s. Specific impulse sea level: 260 s. Diameter: 0.10 m (0.32 ft).

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

Family: Storable liquid. Country: China. Propellants: N2O4/UDMH. Agency: Beijing Wan Yuan.

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