J-8I Multipurpose fighter

J-8I Multipurpose fighter. First flight: 1961 (1981)
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In numbers  Through the lens  Video

Upgraded all-weather interceptor equipped with SR-4 radar. The prototype first flew in 1981 and entered service in 1985.

A total of over 200 J-8s and J-8 I's were built and remain active.




Technical specifications

DESIGNER Chenyang
COUNTRY China
TYPE
Multipurpose fighter
CREW 1
POWER-PLANT Two Liyang (LMC) Wopen-7A turbojet engines
Thrust, kgf  
- with afterburning
2x5.995
- without afterburner
2x4.400
DIMENSIONS
 
Length, m
21,52
Height, m
5,41
Wing span, m
9,34
Wing area m2
42,00
WEIGHT  
Maximum take-off, kg 16.580
Normal take-off, kg 13.700
Empty aircraft, kg 9.285
Internal fuel, kg 4.600
Weight of transported fuel with external tanks, l -
Warload, kg  4.500
PERFORMANCE  
Maximum speed, km/h 2.332
Cruising speed, km/h 850
Maximum speed in low height, km/h -
Combat range, km
800
Range, km 1.500
Ferry range, km 2.000
Service ceiling, m 20.800
Rate of climb, m/min 9.780
Maximum overload, g 4
ARMAMENT A twin-cannon type 23-3 (GSh-23L) 23 mm, with 200 rounds or one NR-30 cannon. Number external hardpoints: 5-7. Transportation of weapons: PL-2B, PL-5B, PL-3 air-to-air missiles, 2 aerial bombs of 500 and 250 kg or Qimgan 12x57 mm or 7x90 mm rocket launchers.