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No known major achievements
J-8 Finback Specifications
Primary Function:Intercept
Contractor:People’s Republic of China (PRC) — Shenyang
Crew:One
Unit Cost:N/A
Powerplant
Two Wopen 13A-II turbojets rated at 14,815 lbst thrust
Dimensions
Length:70 ft 10 in (21.6 m)
Wingspan:30 ft in ( 9.3 m)
Height:17 ft 9 in ( 5.4 m)
Weights
Empty:21,600 lb (9,820 kg)
Maximum Takeoff:39,200 lb (17,800 kg)
Performance
Speed:1,450 mph (2,340 km/h / Mach 2.2)
Ceiling:18-20,000 meters
Range:700 nm (1300 km) cruise radius
Armament
Two 23mm Cannon; one underfuselage hardpoint; six underwing hardpoints for fuel, bombs, rockets, or missiles; drop tanks
Service Life
First Flight:July 5, 1969 (prototype)
April 24, 1981 (J-8I prototype)
June 12, 1984 (J-8II prototype)
March 31, 1996 (J-8IIM prototype)
End of Service:N/A
Number Built:[~130 total]
J-8 Finback Achievements
No known major achievements
