In numbers Through the lens Video
J-11(derived from the Soviet-designed Sukhoi Su-27). Single-seat, twin-engine multi-role air superiority fighter equipped with Al-31F engines, total thrust 25,000 kgf. It first flew in 1977, and as the J-11 in 1992.
Also manufactured under license from Shenyang.
Technical specifications
| DESIGNER | Chenyang (OKB Sukhoi) |
| COUNTRY | China, Russia |
| TYPE |
Multipurpose fighter
|
| CREW | 1 |
| POWER-PLANT | Two Woshan WS-10A Taihang turbofan engines |
| Thrust, kgf | |
|
- with afterburning
|
2x13.460 |
|
- without afterburner
|
2x9.092 |
|
DIMENSIONS
|
|
|
Length, m
|
21,935
|
|
Height, m
|
5,932
|
|
Wing span, m
|
14,70
|
| Wing area m2 |
62,037
|
| WEIGHT | |
| Maximum take-off, kg | 33.000 |
| Normal take-off, kg | 23.926 |
| Empty aircraft, kg | 16.380 |
| Internal fuel, kg | 7.500 |
| Weight of transported fuel with external tanks, l | - |
| Warload, kg | 6.000 |
| PERFORMANCE | |
| Maximum speed, km/h | 2.500 |
| Cruising speed, km/h | - |
| Maximum speed in low height, km/h | - |
|
Combat range, km
|
- |
| Range, km | 1.340 |
| Ferry range, km | 3.530 |
| Service ceiling, m | 18.500 |
| Rate of climb, m/min | 18.000 |
| Maximum overload, g | 9 |
| ARMAMENT | One 30 mm cannon GSh-301, with 150 rounds. Number external hardpoints: 10. Possibility of transport up to 6 air-to-air missile R-27ER1 or R-27ET1 or R-27EΤΕ or R-27ERΕ or 4xR-73. |