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

Status: Retired 1981. Thrust: 3,000.00 kN (674,400 lbf). Gross mass: 150,400 kg (331,500 lb). Unfuelled mass: 10,000 kg (22,000 lb). Specific impulse: 289 s. Specific impulse sea level: 258 s. Burn time: 128 s. Height: 20.10 m (65.90 ft). Diameter: 3.35 m (10.99 ft). Span: 3.35 m (10.99 ft).

Cost $ : 4.000 million. No Engines: 4.



Country: China. Engines: YF-20A. Launch Vehicles: Dong Feng 5, Feng Bao 1, Chang Zheng 2. Propellants: N2O4/UDMH.

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