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MILAVIA > Aircraft > FC-1/JF-17 > Specifications Last updated: 17 November 2007
FC-1/JF-17 THUNDER


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Technical Specifications FC-1/JF-17

Powerplant: one 49.4 kN (11,103 lb st) dry or 84.4 kN (18,969 lb st) with afterburner Klimov RD-93 turbofan or equivalent co-produced WS-13 turbofan.

Dimensions: length 14.97 m (49 ft 1 1/2 in); height 4.77 m (15 ft 8 in); wing span 9.46 m (31 ft 1/2 in)

Weights: empty 6,411 kg (14,136 lb); Normal Take-Off Weight 9,072 kg (20,000 lb); Max Take-Off Weight 12,474 kg (27,500 lb)

Performance: max level speed 'clean' at altitude Mach 1.6 or 1,909 km/h (1,186 mph); service ceiling 15,240 m (50,000 ft); ferry range 2,037 km (1,266 miles); operational radius 1,352 km (840 miles); G-limit: +8.5

Armament: one internal GSh-23-2 twin-barrel 23mm cannon; up to 3,629 kg (8,000 lb) of ordnance including PL-7, PL-10, R550 Magic-2, A-Darter, PL-5C, AIM-9L/P, Mica, Aspide, air-to-air missiles, AM-39 Exocet anti-ship missile, Mk.82 Mk.84 GBU-10, GBU-12, Durandel, Rockeye, and Chinese equivalent air-to-ground weapons, unguided rockets, auxiliary fuel tanks, carried on up to 7 external stations. Two wingtip station, four underwing and one centerfuselage.

FC-1/JF-17 Specifications differ from source to source. Please report any corrections or updates with reliable source, webmaster@milavia.net





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