J-8IIA (J-8D) Multipurpose fighter

J-8IIA (J-8D) Multipurpose fighter. First flight: 1996
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In numbers  Through the lens  Video

Naval version, equipped with aerial refueling system.

It is an evolution of the aircraft incorporating the improved KLJ-1 radar. Xian 563B inertial navigation satellite system and JD-3II TACAN HUD radio navigation system etc.

In 1996 he joined the service.




Technical specifications

DESIGNER Chenyang
COUNTRY China
TYPE
Multipurpose fighter
CREW 1
POWER-PLANT Two Liyang Wopen-13AII (R-13-300) turbojet engines. 
Thrust, kgf  
- with afterburning
2x6.719
- without afterburner
2x4.350
DIMENSIONS
 
Length, m
21,59
Height, m
5,41
Wing span, m
9,344
Wing area m2
42,20
WEIGHT  
Maximum take-off, kg -
Normal take-off, kg 14.300
Empty aircraft, kg 9.830
Internal fuel, kg 5.400
Weight of transported fuel with external tanks, l -
Warload, kg  4.500
PERFORMANCE  
Maximum speed, km/h 2.300
Cruising speed, km/h -
Maximum speed in low height, km/h -
Combat range (with an external tanks), km
800
Range (with an external tanks), km 2.200
Service ceiling, m 19.000
Rate of climb, m/min 12.000
Maximum overload, g 8
ARMAMENT A twin-cannon type 23-3 (GSh-23L) 23 mm, with 200 rounds. Number external hardpoints: 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.