J-10 Multipurpose fighter-bomber

J-10 Multipurpose fighter-bomber. First flight: 1988
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Three-view drawing

J-10 Multipurpose fighter-bomber © Konstantinos Panitsidis




Technical specifications

DESIGNER Chengdu
COUNTRY China
TYPE
Multipurpose fighter-bomber
CREW 1
POWER-PLANT One AL-31FN turbofan engine
Thrust, kgf  
- with afterburning
1x12.500
- without afterburner
1x7.600
DIMENSIONS
 
Length, m
14,57
Height, m
4,78
Wing span, m
8,78
Wing area m2 33,05
WEIGHT  
Maximum take-off, kg -
Normal take-off, kg 18.000
Empty aircraft, kg 9.800
Internal fuel, kg 2.625
Weight of transported fuel with external tanks, l 4.165
Warload, kg  7.260
PERFORMANCE  
Maximum speed, km/h 2.450
Cruising speed, km/h 1.110
Maximum speed in low height, km/h -
Combat range, km
-
Range, km 2.000
Service ceiling, m 18.000
Rate of climb, m/min -
Maximum overload, g 9
ARMAMENT One 23 mm cannon. Number external hardpoints: 11. Transportation of weapons: Air-to-air missiles PL-8, PL-10, PL-11, R-27 or P-73, also air-to-surface missiles. Unguided rockets, free-fall bombs, etc.