YF-3

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YF-3

Part of YF-1

Beijing Wan Yuan N2O4/UDMH rocket engine. Out of production. Used on CZ-1D launch vehicle. First flight 1995.

Status: Out of production. Number: 3 . Thrust: 294.00 kN (66,093 lbf). Specific impulse: 287 s. Specific impulse sea level: 260 s. Burn time: 120 s. Diameter: 2.25 m (7.38 ft).

Thrust (sl): 266.300 kN (59,867 lbf). Thrust (sl): 27,160 kgf. Thrust to Weight Ratio: 0.

Family: Storable liquid. Country: China. Launch Vehicles: Chang Zheng 1D. Propellants: N2O4/UDMH. Stages: CZ-1D-2. Agency: Beijing Wan Yuan.

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