F-16 Fighting Falcon
The General Dynamics F-16 Fighting Falcon is an American single-engine supersonic multirole fighter aircraft originally developed by General Dynamics for the United States Air Force (USAF). Designed as an air superiority day fighter, it evolved into a successful all-weather multirole aircraft with over 4,600 built since 1976.[4] Although no longer purchased by the U.S. Air Force, improved versions are being built for export.
The Fighting Falcon's key features include a frameless bubble canopy for enhanced cockpit visibility, a side-mounted control stick to ease control while maneuvering, an ejection seat reclined 30 degrees from vertical to reduce the effect of g-forces on the pilot, and the first use of a relaxed static stability/fly-by-wire flight control system that helps to make it an agile aircraft. The F-16 has an internal M61 Vulcan cannon and 11 hardpoints.
Specifications
General Characteristics
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- Wingspan 33.8ft (10.3m)
- Length 33.7ft (10.3m)
- Height 12.5ft (3.8m)
- Empty Weight 9,931lbs (4,504kg)
- Loaded Weight 16,340lbs (7,411kg)
Performance
- Power/Weight Ratio 2.062
- Wing Loading 77.8lbs/ft2 (380.1kg/m2)
- Wing Area 209.9ft2 (19.5m2)
- Drag Points 2354
Parts
- Number of Parts 37
- Control Surfaces 5
- Performance Cost 314
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