The FC-1/JF-17 is a lightweight, single-engine, multipurpose combat aircraft developed jointly by the Pakistan Aeronautical Complex (PAC) and Chengdu Aircraft Corporation (CAC) of China. It was designed and developed as a fourth-generation fighter. The FC-1/JF-17 can deploy diverse ordnance, including air-to-air, air-to-surface, and anti-ship missiles, guided and unguided bombs, and a 23 mm GSh-23-2 twin-barrel autocannon.
Specifications
General Characteristics
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- Wingspan 26.7ft (8.1m)
- Length 33.9ft (10.3m)
- Height 12.6ft (3.8m)
- Empty Weight 6,146lbs (2,787kg)
- Loaded Weight 10,421lbs (4,727kg)
Performance
- Power/Weight Ratio 3.234
- Wing Loading 43.2lbs/ft2 (211.0kg/m2)
- Wing Area 241.2ft2 (22.4m2)
- Drag Points 1993
Parts
- Number of Parts 52
- Control Surfaces 5
- Performance Cost 359
