Shenyang J-11A

Specifications

General characteristics

Crew: 1

Length: 21.9 m (71 ft 10 in)

Wingspan: 14.70 m (48 ft 3 in)

Height: 5.92 m (19 ft 6 in)

Wing area: 62.04 m² (667.8 ft²)

Empty weight: 16,870 kg [1] (37,192 lb)

Loaded weight: 23,140 kg (51,010 lb)

Max takeoff weight: 33,000 kg (73,000 lb)

Powerplant: 2× Lyulka AL-31F or Woshan WS-10A "Taihang" turbofans

Dry thrust: 74.5 kN / 89.17 kN (16,800 lbf / 20,050 lbf)[12] each

Thrust with afterburner: 123 kN / 129.4 kN (27,600 lbf / 29,101 lbf) [13] each

Performance

Maximum speed: Mach 2.35 (2,500 km/h, 1,600 mph) at altitude

Range: 3,720 km (2,010 nm, 2,310 mi)

Combat radius: 2,000 km (1,240 mi)

Service ceiling: 19,000 m (62,523 ft)

Rate of climb: >325 m/s (64,000 ft/min)

Wing loading: 371.0 kg/m² (76 lb/ft²)

Thrust/weight: Dry: 0.66 / With afterburner: 1.09

G-limit: 9 g

Armament

Guns: 1× 30 mm (1.18 in) Gryazev-Shipunov GSh-30-1 cannon with 150r

Hardpoints: 10: 2 under fuselage, 2 under air ducts, 4 under wings, 2 on wingtips and provisions to carry combinations of:

Missiles:

PL-12

PL-9

PL-8

Vympel R-77

Vympel R-27

Vympel R-73

Rockets: Unguided rocket launcher

Bombs: Free-fall cluster bombs

Avionics

Fire-control radar: NIIP Tikhomirov N001VE Myech coherent pulse Doppler radar

OEPS-27 electro-optic system

NSts-27 helmet-mounted sight (HMS)

Gardeniya ECM pods


Data from Sino Defense.com.
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