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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.