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J-16
Role Multirole fighter
National origin People's Republic of China
Manufacturer Shenyang Aircraft Corporation
Introduction 2013 [1]
Status In service
Primary user People's Liberation Army Air Force
Developed from Shenyang J-11BS

The Shenyang J-16 fighter/bomber is a new strike plane designed and manufactured by Shenyang Aircraft Corporation, China. This is a multi-role fighter/bomber variant based on the J-11BS with longer range and upgraded avionics, the concept is similar to F-15E fighter/bomber. The first few photos of J-16 were published on Chinese internet websites around June 2012. It appears J-16 has a slightly different vertical stabilizer compared to J-11 fighter or J-15 naval fighter. It is also equipped with missile pylons for Chinese PL-8 air-to-air missiles, another difference compared to earlier J-11 variants.

Like the J-11BS and the J-15, the fighter features numerous enhancements such as an AESA radar from the 607th institute (the same manufacturer of the AESA found on the J-11B and J-15), composites, radar absorbent material, MAWS, WS-10, ECM upgrades, and more.[2]

According to media reports, China has developed Shenyang J-16 fighter based on the Shenyang J-11 airframe influenced by the Russian Sukhoi Su-30MKK that was sold to China in 2000.[3][4]

Specifications[]

General characteristics

  • Crew: 2
  • Length: 21.9 m (72 ft)
  • Wingspan: 14.7 m (48.25 ft)
  • Height: 6.36 m (20.85 ft)
  • Wing area: 62.04 m2 (667.80 ft2)
  • Empty weight: 17,700 kg (38,600 lb)
  • Loaded weight: 26,000 kg (58,000 lb)
  • Max. takeoff weight: 35,000 kg (77,000 lb)
  • Powerplant: 2 × WS-10A afterburning turbofans
    • Dry thrust: 89.17 kN (20,050 lbf) each
    • Thrust with afterburner: 135 kN (33,000 lbf) each

Performance

  • Maximum speed: Mach 2.0
  • Range: 3000 km (1900 mi)
  • Ferry range: 4000 km()
  • Service ceiling: 17,300 m (56,800 ft)
  • Rate of climb: 305 m/s ()

Armament

  • 1 × 30 mm GSh-30-1 cannon with 150 rounds
  • Munitions on twelve external hardpoints, including:
  • See also[]

    References[]

    External links[]



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