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 26.8ft (8.2m)
- Length 33.9ft (10.3m)
- Height 12.6ft (3.8m)
- Empty Weight 6,843lbs (3,104kg)
- Loaded Weight 11,119lbs (5,043kg)
Performance
- Power/Weight Ratio 3.031
- Wing Loading 46.1lbs/ft2 (225.1kg/m2)
- Wing Area 241.2ft2 (22.4m2)
- Drag Points 1993
Parts
- Number of Parts 48
- Control Surfaces 5
- Performance Cost 319
