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Fighter

J-10 (Prototype Development)

Chengdu · China

While secret at the time, 1997 was a critical year for the J-10 flight test program. Utilizing a canard-delta wing design (partially influenced by the cancelled Israeli Lavi), it represented China's jump into modern, fly-by-wire multi-role fighter production.

Technical Specifications
First Flight 1997
Max Speed 2,327 km/h (Mach 1.8)
Range 1,850 km
Ceiling 18,000 m
Engines 1x Saturn AL-31FN afterburning turbofan
Armament & Payload

1x 23mm GSh-23; 11 hardpoints for PL-8/PL-10 missiles.