In numbers Through the lens Video
Technical specifications
| DESIGNER | Chenyang |
| COUNTRY | China |
| TYPE |
Multipurpose fighter
|
| CREW | 1 |
| POWER-PLANT | Two Liyang Wopen-13AII (R-13-300) turbojet engines. |
| Thrust, kgf | |
|
- with afterburning
|
2x6.719 |
|
- without afterburner
|
2x4.350 |
|
DIMENSIONS
|
|
|
Length, m
|
21,59
|
|
Height, m
|
5,41
|
|
Wing span, m
|
9,344
|
| Wing area m2 |
42,20
|
| WEIGHT | |
| Maximum take-off, kg | - |
| Normal take-off, kg | 14.300 |
| Empty aircraft, kg | 9.830 |
| Internal fuel, kg | 5.400 |
| Weight of transported fuel with external tanks, l | - |
| Warload, kg | 4.500 |
| PERFORMANCE | |
| Maximum speed, km/h | 2.300 |
| Cruising speed, km/h | - |
| Maximum speed in low height, km/h | - |
|
Combat range (with an external tanks), km
|
800 |
| Range (with an external tanks), km | 2.200 |
| Service ceiling, m | 19.000 |
| Rate of climb, m/min | 12.000 |
| Maximum overload, g | 8 |
| ARMAMENT | A twin-cannon type 23-3 (GSh-23L) 23 mm, with 200 rounds. Number external hardpoints: 7. Transportation of weapons: PL-2B, PL-5B, PL-3 air-to-air missiles, 2 aerial bombs of 500 and 250 kg or Qimgan 12x57 mm or 7x90 mm rocket launchers. |