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J-7E Multipurpose fighter

J-7E Multipurpose fighter. First flight: 1990
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In numbers  Through the lens  Video

The J-7E prototype first flew in 1990 and was fitted with a delta wing to improve its performance. Armament includes two internal 30mm guns with 60 rounds each and is similar to the F-7PG version.

In 1993, he joined the Chinese Air Force.




Technical specifications

DESIGNER Chengdu
COUNTRY China
TYPE
Multipurpose fighter
CREW 1
POWER-PLANT One LMC WP-13F turbojet engine
Thrust, kgf  
- with afterburning
1x6.500
- without afterburner
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DIMENSIONS
 
Length, m
13,95
Height, m
4,11
Wing span, m
8,32
Wing area m2
24,88
WEIGHT  
Maximum take-off, kg 9.100
Normal take-off, kg 7.540
Empty aircraft, kg 5.292
Internal fuel, kg 2.385
Weight of transported fuel with external tanks, l 1.780 (2x480 or 1x800 or 500)
Warload, kg  1.400
PERFORMANCE  
Maximum speed, km/h 2.175
Maximum speed in low height, km/h -
Combat range, km
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Ferry range, km 2.200
Service ceiling, m 17.500
Rate of climb, m/min 11.700
Maximum overload, g 8
ARMAMENT Two 30 mm cannons Type 30-1 with 60 rounds. Number external hardpoints: 5. Possibility of transport up to 4 air-to-air missile PL-2, PL-2A, PL-7 and PL-9. 4 x air-to-air missile Magic R550 or AIM-9P Sidewinder. 2-4 launcher HF-7C (18x57 mm), Type 90-1 (7x90) or 2 bombs 500 kg or 4 bombs 250 kg or 10 bombs 100 kg.