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Introduction | Specifications | Design and Avionics | Powerplant | Weaponry | Engines | Programme History | J-10B Fighter-Trainer | Deployment | Gallery Specifications* Crew: 1 * Length: 14.57 m (47.86 ft) * Wingspan: 8.78 m (28.75 ft) * Height: 4.80 m (15.75 ft) * Wing area: 33.00 m² (355.2 ft²) * Empty weight: 9,750 kg (21,500 lb) (some sources say 6,940 kg (15,300 lb)) * Useful load: 4,500 kg (9 920 lb) * Maximum gross takeoff weight: 18,400 kg (40,565 lb) * Powerplant: 1× Lyulka-Saturn AL-31FN turbofan, rated at 79.43 kN dry, 122.58 kN with afterburning (17,857 lbf, 27,557 lbf) Performance * Maximum speed: Mach 1.2 at sea level; Mach 2.0 at altitude (1470 km/h, 913.4 mph; 2450 km/h, 1522 mph) * g-Limits: +9/-3 g (+88/-29 m/s², +290/-97 ft/s²) * Range: o Combat radius: 550 km (300 nm, 340 mi) o Maximum range: 1,850 km (1,000 nm, 1,150 mi) * Service ceiling: 18,000 m (59,055 ft) * Rate of climb: m/s (ft/min) * Wing loading: kg/m² (lb/ft²) * Thrust/weight: at least 1:1 Armament * Guns: 1× 23 mm internal cannon * Hardpoints: 11, 3 under each wing and 5 under the fuselage * Missiles: o Air-to-air: PL-8, PL-11, PL-12, R-73, R-77 o Air-to-surface: YJ-9, YJ-9K * Bombs: laser-guided bombs, unguided bombs Source: Wikipedia |