johnbr

J-10

Specifications (J-10A)General characteristics Crew: 1 (basic), 2 (trainer variant)[11] Length: 16.43 m [27] (53 ft 10 in) Wingspan: 9.75 m [27] (31 ft 11 in) Height: 4.78 m (15.7 ft) Wing area: 39 m² (419.8 ft²) Empty weight: 9,750 kg (21,495 lb [40]) Loaded weight: 14,876 kg (32,797 lb) Useful load: 4,500 kg[41][42] (9,920 lb) Max takeoff weight: 19,277 kg (42,500 lb[11]) Powerplant: 1 × Saturn-Lyulka AL-31FN or WS-10A Taihang turbofan Dry thrust: 79.43 kN / 89.17 kN (17,860 lbf / 20,050 lbf) Thrust with afterburner: 122.5 kN[11] / 132 kN (27,557 lbf / 29,101 lbf) Performance Maximum speed: Mach 2.2 at altitude,[27][43] Mach 1.2 at sea level[7] g-limits: +9/-3 g (+88/-29 m/s², +290/-97 ft/s²[7]) Combat radius: 1600 km[44] with in-flight refueling 1100 km without in flight refueling[33] () Ferry range: 3200 km [33] () Service ceiling: 20,300 m [33] (66,601 ft [33][45]) Wing loading: 335 kg/m² (69 lb/ft²) Thrust/weight: 0.98 (with AL-31); 1.03 (with WS-10A) Armament Guns: 1× 23mm twin-barrel cannon Hardpoints: 11 in total (6× under-wing, 5× under-fuselage) with a capacity of 6,000 kg (13,228 lb) external fuel and ordnance [30] Rockets: 90 mm unguided rocket pods Missiles: Air-to-air missiles: PL-8, PL-9, PL-11, PL-12 Air-to-surface missiles: PJ-9, YJ-9K Bombs: laser-guided bombs (LT-2), glide bombs (LS-6) and unguided bombs

J-10
johnbr, Sep 22, 2011
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  • Category:
    Modern Aircraft
    Uploaded By:
    johnbr
    Date:
    Sep 22, 2011
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