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FB-1-2
Part of CZ-2-2 stage series
N2O4/UDMH propellant rocket stage. .

Status: Retired 1981. Thrust: 761.90 kN (171,282 lbf). Gross mass: 38,300 kg (84,400 lb). Unfuelled mass: 3,500 kg (7,700 lb). Specific impulse: 295 s. Specific impulse sea level: 270 s. Burn time: 127 s. Height: 7.40 m (24.20 ft). Diameter: 3.35 m (10.99 ft). Span: 3.35 m (10.99 ft).

Cost $ : 2.000 million.



Country: China. Engines: YF-22/23. Launch Vehicles: Dong Feng 5, Feng Bao 1, Chang Zheng 2. Propellants: N2O4/UDMH.

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