Feng Bao 1

Function	Carrier rocket
Country of origin	China
Size
Height	33 metres (108 ft)
Diameter	3.35 metres (11.0 ft)
Mass	191,700 kilograms (422,600 lb)
Stages	Two
Capacity
Payload to LEO
Mass	2,500 kilograms (5,500 lb)
Launch history
Status	Retired
Launch sites	Jiuquan LA-2B
Total launches	11
Success(es)	7
Failure(s)	4
First flight	10 August 1972
Last flight	19 September 1979
Type of passengers/cargo	JSSW
First stage
Powered by	4 YF-20A
Maximum thrust	3,000 kilonewtons (670,000 lbf)
Specific impulse	289 sec
Burn time	128 seconds
Propellant	N2O4/UDMH
Second stage
Powered by	1 YF-22; 4 YF-23
Maximum thrust	761.9 kilonewtons (171,300 lbf)
Specific impulse	295 sec
Burn time	127 seconds
Propellant	N2O4/UDMH
	[edit on Wikidata]

The Feng Bao 1 (Chinese: 风暴, meaning Storm), also known as FB-1, was a Chinese carrier rocket launched between 1972 and 1981. It was replaced by the nearly identical Long March 2, which had been developed at the same time for political reasons related to China's Cultural Revolution.^[1]

The Feng Bao was derived from the DF-5 missile. Eleven were launched, of which four failed.^[2] Launches occurred from LA-2B at the Jiuquan Satellite Launch Centre.

Launch history

Date/Time (GMT)	S/N	Payload	Outcome	Remarks
10 August 1972 00:32^[3]	701-02	Shiyan Peizhong	Successful	Suborbital test, apogee: 200 kilometres
18 September 1973 12:12^[3]	701-03	JSSW-1	Failure
12 July 1974 13:55^[3]	701-04	JSSW-2	Failure	Loss of attitude control^[1]
26 July 1975 13:28^[1]	701-05	JSSW-3	Successful
16 December 1975 09:19^[1]	701-06	JSSW-4	Successful
30 August 1976 11:53^[1]	701-07	JSSW-5	Successful
10 November 1976 09:05^[3]	701-08	JSSW-6	Failure
14 September 1977 00:15^[3]	701(II)-01	DDDS	Successful	Suborbital test, apogee: 200 kilometres
16 April 1978 16:39^[3]	701(II)-02	DDDS	Successful	Suborbital test, apogee: 200 kilometres
27 July 1979 21:28^[3]	XCZ-1-02	Shi Jian 1	Failure	Second stage malfunction
19 September 1981 21:28:40^[3]	XCZ-1-02	Shi Jian 2	Successful	Payload consisted of three satellites

References

^ ^a ^b ^c ^d ^e Wade, Mark. "CZ". Encyclopedia Astronautica. Retrieved 2009-01-25.
^ Krebs, Gunter. "FB-1 (Feng Bao-1)". Gunter's Space Page. Retrieved 2009-01-25.
^ ^a ^b ^c ^d ^e ^f ^g ^h McDowell, Jonathan. "DF-5". Launch vehicles database. Jonathan's Space Page. Retrieved 2009-01-25.

[EA-CZ-1] Wade, Mark. "CZ". Encyclopedia Astronautica. Retrieved 2009-01-25.

[GSP-2] Krebs, Gunter. "FB-1 (Feng Bao-1)". Gunter's Space Page. Retrieved 2009-01-25.

[JSR-3] ^ ^a ^b ^c ^d ^e ^f ^g ^h McDowell, Jonathan. "DF-5". Launch vehicles database. Jonathan's Space Page. Retrieved 2009-01-25.

[1]

[2]

[3]

v t e Orbital launch systems
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Current	Angara 1.2 A5 Ariane 6 Atlas V Ceres 1 1S Chollima-1 Electron Falcon 9 Block 5 Falcon Heavy Firefly Alpha Gravity-1 GSLV H-IIA H3 Hyperbola-1 Jielong 1 3 KAIROS^† Kaituozhe 2 Kinetica 1 Kuaizhou 1 1A 11 Long March 2C 2D 2F 3A 3B/E 3C 4B 4C 5 5B 6 6A 7 7A 8 11 11H 12 LVM3 Minotaur I IV V C Nuri OS-M1^† Pegasus XL Proton-M PSLV Qaem 100 Qased Shavit 2 Simorgh SLS Block 1 Soyuz-2 2.1a / STA 2.1b / STB 2-1v SSLV Starship Tianlong-2 Unha Vega C Vulcan Centaur Zhuque 2
In development	Antares 330 Bloostar Cyclone-4M Deca Epsilon S Eris Gravity-2 Hyperbola-2 Irtysh Kuaizhou 21 31 Long March 9 10 Miura 5 MLV Neutron New Glenn New Line 1 NGLV Nova OS-M 2 4 Orbex Prime Pallas-1 Red Dwarf SLS Block 1B Block 2 Soyuz-7 Terran R Tianlong-3 VLM Vega E Zero Zhuque 3 Zuljanah
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Classes	Sounding rocket Small-lift launch vehicle Medium-lift launch vehicle Heavy-lift launch vehicle Super heavy-lift launch vehicle
This Template lists historical, current, and future space rockets that at least once attempted (but not necessarily succeeded in) an orbital launch or that are planned to attempt such a launch in the future Symbol ^† indicates past or current rockets that attempted orbital launches but never succeeded (never did or has yet to perform a successful orbital launch)

Launch history

See also

References