Modern Drawings/Air/China/Fighters/J-11/J-11B.htm | Update: -

 

 

PLAAF - No additional information

 

 

Specifications

General

Type: Air-superiority fighter, multirole fighter
Crew: 1
First flight: 1998
Introduction: 1998
Number built: 253+ (as of February 2014)
Powerplant
2 × Lyulka AL-31F or Woshan WS-10A "Taihang" turbofans
Dry thrust: 75.22 kN / 89.17 kN each
Thrust with afterburner: 23 kN / 132 kN each
Dimensions/Masses
Length: 21.9 m | Wingspan: 14.7 m | Height: 5.92 m
Wing area: 62 m² | Empty weight: 16380 kg
Max. takeoff weight: 33000 kg
Performances
Maximum speed: : Mach 2.35 (2500 km/h) at altitude
Service ceiling: 19000 m
Range: 3530 km at altitude; (1340 km at sea level)
Armament

Inside: 1 × 30 mm GSh-30-1 cannon with 150 rounds
Outside: 10: 2 under fuselage, 2 under air ducts, 4 under wings, 2 on wingtips and provisions to carry combinations of missiles, rockets & bombs

 

 

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