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Feng Bao 1
Part of CZ
FB-1 Launch
FB-1 Launch
Chinese orbital launch vehicle. The FB-1, like the CZ-2 launch vehicle begun the following year, was a two-stage booster developed from the DF-5 intercontinental ballistic missile. Payload for the booster was the JSSW, believed to have been a television-transmission military reconnaissance satellite. The incredible decision to develop two nearly identical rockets concurrently can be blamed on the turbulent factional politics after the Cultural Revolution.

AKA: FB-1;Feng-Bao-1;Storm 1. Status: Retired 1981. First Launch: 1972-08-10. Last Launch: 1981-09-19. Number: 11 . Payload: 2,500 kg (5,500 lb). Thrust: 2,679.00 kN (602,263 lbf). Gross mass: 191,700 kg (422,600 lb). Height: 33.00 m (108.00 ft). Diameter: 3.35 m (10.99 ft). Apogee: 200 km (120 mi).

The 'Gang of Four' was formed by Mao Zedong's wife Jiang Qing, a Shanghai Propaganda Department official, a literary critic, and a Shanghai security guard. They rose to power during turbulent period of the Cultural Revolution (1966-1976) and dominated Chinese politics during that time. Development of the FB-1 (Feng Bao-1 = Storm-1), the first Chinese heavy-lift launch vehicle, began under their auspices in the autumn of 1969. A development team was formed with the Shanghai No. 2 Bureau of Mechanic-Electrical Industry as the leader. General system design was started in December the same year.

After Mao's death in September 1976, the Gang of Four was arrested and orbital flights of the FB-1 and JSSW came to a halt. In 1980 the Gang of Four were tried in court and given lengthy prison sentences. The final FB-1 made its last flight a year later with a payload of assorted scientific satellites. The FB-1 had slightly lower performance than the CZ-2 and no useful results from the series of JSSW satellites launched have been reported. However the Shanghai facility remained in use, being assigned development of the CZ-4 variants of the triumphant CZ-2 design.

LEO Payload: 2,500 kg (5,500 lb) to a 200 km orbit. Flyaway Unit Cost 1985$: 6.000 million.

Stage Data - FB-1



Family: orbital launch vehicle. Country: China. Engines: YF-22/23, YF-20A. Spacecraft: JSSW, SJ. Launch Sites: Jiuquan, Jiuquan LA2B. Stages: FB-1-1, FB-1-2. Agency: CALT.
Photo Gallery

FB-1 EngineFB-1 Engine


FB-1FB-1


Chinese RV TestChinese RV Test
Test of low drag Chinese re-entry vehicle, 1998.
Credit: Richard D. Fisher, Jr


FB-1FB-1


FB-1FB-1



1972 August 10 - . 00:32 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Feng Bao 1.
1973 September 18 - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Feng Bao 1. FAILURE: Failure. Failed Stage: U.
1974 July 14 - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Feng Bao 1. FAILURE: Vehicle lost attitude stability and destroyed by range safety.. Failed Stage: G.
1975 July 26 - . 13:28 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Feng Bao 1.
1975 December 16 - . 09:19 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Feng Bao 1.
1976 August 30 - . 11:53 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Feng Bao 1.
1976 November 10 - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Feng Bao 1. FAILURE: Failure. Failed Stage: U.
1977 September 14 - . 00:15 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Feng Bao 1.
1978 April 15 - . 16:39 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Feng Bao 1.
1979 July 28 - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Feng Bao 1. FAILURE: Second stage failure.. Failed Stage: 2.
1981 September 19 - . 21:28 GMT - . Launch Site: Jiuquan. Launch Complex: Jiuquan LA2B. LV Family: CZ. Launch Vehicle: Feng Bao 1.

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