J-10CE Fighter

Übersicht

J-10CE fighter is an all-weather multi-role advanced fighter aircraft with single seat and single engine, derived from J-10C aircraft. J-10CE fighter has powerful Co-operative Engagement Capability (CEC), advanced Beyond Visual Range (BVR) attack capability on multi-targets under strong electromagnetic environment, and precise ground strike capability in multi-modes. J-10CE has remarkable performance in maneuverable dogfight at low and medium altitudes, supersonic flight, short distance take-off and landing, large combat radius, long endurance and air refueling. J-10CE is equipped with advanced integrated avionics and weapon system, with strong weapon capability. Length: 16.9 m (55 ft 5 in) Wingspan: 9.8 m (32 ft 2 in) Height: 5.7 m (18 ft 8 in) Wing area: 37 m2 (400 sq ft) Empty weight: 9,750 kg (21,495 lb) [68][unreliable source?] Gross weight: 14,000 kg (30,865 lb) Max takeoff weight: 19,227 kg (42,388 lb) Fuel capacity: 4950 L (3860 Kg) internal.[68] 4000 L (3120 Kg) external with 3 drop tanks (2x1600L + 1x800L) Powerplant: 1 WS-10B[70] afterburning turbofan engines, 89.17 kN (20,050 lbf) thrust dry, 144 kN (32,000 lbf) with afterburner Stall speed: 200 km/h (120 mph, 110 kn) Range: 1,850 km (1,150 mi, 1,000 nmi) Combat range: 1,240 or 2,600 km (770 or 1,620 mi, 670 or 1,400 nmi) Ferry range: 4,600 km (2,900 mi, 2,500 nmi) Service ceiling: 18,000 m (59,000 ft) Rate of climb: 300 m/s (59,000 ft/min) Wing loading: 381 kg/m2 (78 lb/sq ft) On March 11, 2022, the Pakistan Air Force held an installation ceremony for the first batch of six J-10CEs in Kamla. Pakistani Prime Minister Imran Khan attended the ceremony. This marks that China's new generation of aviation main battle equipment has been officially installed in the Pakistan Air Force, realizing the export of China's new generation of aviation main battle equipment into a system, and it is another important milestone for China's aviation equipment export.

Technische Daten

Wichtige technische Daten: Crew 1, Length 16.9 m (55 ft 5 in), Wingspan 9.8 m (32 ft 2 in), Height 5.7 m (18 ft 8 in), Wing area 37 m2 (400 sq ft), Empty weight 9,750 kg (21,495 lb) [68][unreliable source?], Gross weight 14,000 kg (30,865 lb), Max takeoff weight 19,227 kg (42,388 lb), Fuel capacity 4950 L (3860 Kg) internal.[68] 4000 L (3120 Kg) external with 3 drop tanks (2x1600L + 1x800L), Powerplant 1 WS-10B[70] afterburning turbofan engines, 89.17 kN (20,050 lbf) thrust dry, 144 kN (32,000 lbf) with afterburner, Maximum speed Mach 1.8, Stall speed 200 km/h (120 mph, 110 kn), Range 1,850 km (1,150 mi, 1,000 nmi), Combat range 1,240 or 2,600 km (770 or 1,620 mi, 670 or 1,400 nmi), Ferry range 4,600 km (2,900 mi, 2,500 nmi), Service ceiling 18,000 m (59,000 ft), g limits +9/-3, Rate of climb 300 m/s (59,000 ft/min), Wing loading 381 kg/m2 (78 lb/sq ft), Thrust/weight 1.04.

Technische Daten

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