| Specifications |
| Contractors |
Chengdu Aircraft Industry Group (CAIG)
Pakistan Aeronautical Complex (PAC) | |
|
Projected [1999] | Actual [2004] |
| LENGTH |
13.95 meters | 14.9679 m |
| HEIGHT |
5.02 meters | 4.77485 m |
| WING SPAN |
9.5 meters | 9.4646 m |
| MAX T-O WEIGHT |
12,500 kilograms | 12,474 kg |
| Empty weight |
| 6,411 kg |
| Normal takeoff weight |
| 9,072 kg |
| Maximum landing weight |
| 7,802 kg |
| Fuel weight |
| 2,268 kg |
| Weapons load |
| 3,629 kg |
| Thrust/weight ratio |
| >=0.9 |
| MAX LEVEL SPEED |
1031 knots | Mach 1.6 |
| MAX RANGE / Ferry range |
864 nautical miles | 2,037 km |
| SERVICE CEILING |
16,000 meters | 15,240 m |
| T-O RUN |
500 meters | 609 m |
| LANDING RUN |
700 meters | 823 m |
| Armament |
- 23 mm GSh-23-2 twin-barrel cannon
- 6 - PL-7 AAM
- 6 - PL-10 AAMs
- ASMs, bombs
|
- 23 mm double barrel gun
Air-to Surface
- Air to sea missiles
- MAR-1 Anti Radiation Missile
- C-802AK Multirole Attack Cruise Missile
- Raad Stealth Stand off Cruise Missile (Nuclear Capable)
- CM-400AKG Hypersonic Carrier Killer
- CBU-100 Anti Armor Cluster Bombs
- GBU-10/12 LT-2 Laser Guided Smart Munitions
- LS-6 GPS Guided Direct Attack Munitions.
- Hafr-4 Anti Runway Bomb
- Hafr-2 Electro Optical Guided Glide Bomb
- LS-Series Satellite Guided Glide Munitions
- Takbir Satellite Guided Stand off Munition
- General purpose bombs
- Training bombs
Air-to-Air
- 70-100 Km range beyond visual range active missiles
- SD-10A Beyond Visual Range Air to Air Missile
- Highly agile Imaging infrared short range missiles
|
| Avionics | |
- Dual redundant mission computers
- Dual redundant 1553 Mux bus architecture
- Multi-mode Pulse Doppler Radar capable of tracking multiple targets with prioritized firing
- Ring laser gyro inertial navigation system tied with GPS
- Smart head up display with up front control panel. SHUD total field of view is 25 Degrees
- Color video recording camera and video recorder (for SMFCDs)
- HOTAS
- Three smart multi function color displays
- Air Data Computer
- Radar Altimeter
- IFF Interrogator/Transponder
- Air Combat Manoeuvring Instrumentation (ACMI)
- BVR/Communication Data link
- VHF / UHF Communication System
|
| Aerodynamic Configuration | |
- Bifurcated side air inlet with incorporation of latest
BUMP intake technology for improved performance
- Leading edge maneuvering flaps
- Trailing edge flaps
- Twin Ventral Fins
|
| Landing Gear/b> | |
- Nose gear with steering
- Main gear with paddle controlled hydraulic brakes and
anti-skid braking system.
|
| Cockpit Systems | |
- NVG compatible cockpit conforming to US MIL
Standard, suitable for 3% to 98% percentile range of pilots.
- Single Piece Stretch Acrylic Transparent Canopy
providing a good all around Field of Vie
- Ejection Seat
- a- Latest Martin Baker high performance ejection seat
- b- Canopy Severance System for additional safety
- c- French Oxygen Regulation System
- d- Passive Leg Restraint System
Environment Control System and Oxygen System
- Effective control of cockpit pressure and temperature
- Effective temperature and humidity control of cockpit
and avionics for optimum performance
- Efficient Anti G system for Pilot
- Oxygen supply duration three hours
|
| Flight Control | |
- Composite Flight Control System comprising
conventional controls with stability augmentation in roll
and yaw axis and fly by wire in pitch axis
- Quad-redundancy in Fly By Wire System
- Autopilot with Altitude hold and Attitude hold modes
|
| Fuel System | |
- Total internal fuel 5130 lb (3000 liters)
- Single point pressure refueling system
- External Fuel
- a- One centre line drop tank 800 liters
- b- Two under wing drop tanks 800/1100 liters
|
