In numbers Through the lens Video
Chengdu Experimental Fighter (CAC) derived from the J-7II and used as a technology development and systems testing platform for the J-7MF fighter.
Its first flight took place on June 8, 1998.
Technical specifications
| DESIGNER | Chengdu |
| COUNTRY | China |
| TYPE |
Multipurpose fighter
|
| CREW | 1 |
| POWER-PLANT | One LMC WP-13F turbojet engine |
| Thrust, kgf | |
|
- with afterburning
|
1x6.801 |
|
- without afterburner
|
- |
|
DIMENSIONS
|
|
|
Length, m
|
14,89
|
|
Height, m
|
4,11
|
|
Wing span, m
|
7,154
|
| Wing area m2 |
23,00
|
| WEIGHT | |
| Maximum take-off, kg | ~10.000 |
| Normal take-off, kg | 8.200 |
| Empty aircraft, kg | 5.400 |
| Internal fuel, kg | - |
| Weight of transported fuel with external tanks, kg | - |
| Warload, kg | - |
| PERFORMANCE | |
| Maximum speed, km/h | 2.250 |
| Maximum speed in low height, km/h | - |
|
Combat range, km
|
- |
| Range, km | 1.800 |
| Ferry range, km | 2.500 |
| Service ceiling, m | 18.000 |
| Rate of climb, m/min | 11.000 |
| Maximum overload, g | 8,5 |
| ARMAMENT | Doesn't have (defensive). |