This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
 |
Chinese RV Simulatio - Test of low drag Chinese re-entry vehicle, 1998. Credit: Richard D. Fisher, Jr. 14,178 bytes. 269 x 208 pixels. |
|
Family: Long March. Country: China. Status: Hardware.
Launch vehicle derived from DF-5 ICBM. Very similar to CZ-2C.
SpecificationsLaunches: 11. Failures: 4. Success Rate: 63.64% pct. First Launch Date: 10 August 1972. Last Launch Date: 19 September 1981. LEO Payload: 2,500 kg. to: 200 km Orbit. Liftoff Thrust: 273,180 kgf. Total Mass: 191,700 kg. Core Diameter: 3.4 m. Total Length: 33.0 m. Flyaway Unit Cost $: 6.00 million. in 1985 unit dollars.
- Stage Number: 1. 1 x FB-1-1 Gross Mass: 150,400 kg. Empty Mass: 10,000 kg. Thrust (vac): 306,000 kgf. Isp: 289 sec. Burn time: 128 sec. Isp(sl): 258 sec. Diameter: 3.4 m. Span: 3.4 m. Length: 20.1 m. Propellants: N2O4/UDMH No Engines: 4. YF-20A
- Stage Number: 2. 1 x FB-1-2 Gross Mass: 38,300 kg. Empty Mass: 3,500 kg. Thrust (vac): 77,700 kgf. Isp: 295 sec. Burn time: 127 sec. Isp(sl): 270 sec. Diameter: 3.4 m. Span: 3.4 m. Length: 7.4 m. Propellants: N2O4/UDMH No Engines: 1. YF-22/23
FB-1 Chronology
1972 Aug 10 - Launch Site: Jiuquan .
- R&D suborbital
Suborbital.
1973 Sep 18 - LV Configuration: Feng Bao 1 s/n FB1-2. Launch Site: Jiuquan . Launch Complex: LA2. FAILURE: Failure.
- JSSW 1 Spacecraft: JSSW. Payload: JSSW 1.
1974 Jul 14 - LV Configuration: Feng Bao 1 s/n FB1-3. Launch Site: Jiuquan . Launch Complex: LA2. FAILURE: Failure.
- JSSW 2 Spacecraft: JSSW. Payload: JSSW 2.
 | Chinese RV Shapes - Chinese re-entry vehicle shapes, 1998. Credit: Richard D. Fisher, Jr. 17,101 bytes. 331 x 212 pixels. |
1975 Jul 26 - - 13:28 GMT. LV Configuration: Feng Bao 1 s/n FB1-4. Launch Site: Jiuquan . Launch Complex: LA2.
1975 Dec 16 - - 09:19 GMT. LV Configuration: Feng Bao 1 s/n FB1-5. Launch Site: Jiuquan . Launch Complex: LA2.
1976 Aug 30 - - 11:53 GMT. LV Configuration: Feng Bao 1 s/n FB1-6. Launch Site: Jiuquan . Launch Complex: LA2.
- China 6 Spacecraft: JSSW. Payload: JSSW 5. Mass: 1,108 kg.
1976 Nov 10 - LV Configuration: Feng Bao 1 s/n FB1-7. Launch Site: Jiuquan . Launch Complex: LA2. FAILURE: Failure.
- JSSW 6 Spacecraft: JSSW. Payload: JSSW 6.
 | Chinese RV Test - Test of low drag Chinese re-entry vehicle, 1998. Credit: Richard D. Fisher, Jr. 5,979 bytes. 217 x 193 pixels. |
1977 Sep 14 - Launch Site: Jiuquan .
- Research and Development Flight
Suborbital.
1978 Apr 16 - Launch Site: Jiuquan .
- Research and Development Flight
Suborbital.
1979 Jul 28 - LV Configuration: Feng Bao 1 s/n FB1-10. Launch Site: Jiuquan . Launch Complex: LA2. FAILURE: Failure.
- SJ Spacecraft: SJ-1. Payload: SKW. Mass: 221 kg.
1981 Sep 19 - - 21:32 GMT. LV Configuration: Feng Bao 1 s/n FB1-11. Launch Site: Jiuquan . Launch Complex: LA2.
- China 11 Spacecraft: SJ-2A. Mass: 483 kg.
- China 10 Spacecraft: SJ-2C. Mass: 28 kg.
- China 9 Spacecraft: SJ-2B. Mass: 257 kg.
Bibliography:- 42 - Isakowitz, Steven J,, International Reference to Space Launch Systems Second Edition, AIAA, Washington DC, 1991.
- 61 - Wilson, Andrew, editor,, Jane's/Interavia Space Directory, Jane's Information Group, Coulsdon, Surrey, 1992 et al.
Back to Index
Last update 12 March 2001.
Definitions of Technical Terms.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .