Wikipedia The Douglas A-4 Skyhawk is a single-seat subsonic carrier-capable light attack aircraft developed for the United States Navy and United States Marine Corps in the early 1950s. The delta-winged, single turbojet engined Skyhawk was designed and produced by Douglas Aircraft Company, and later by McDonnell Douglas. It was originally designated A4D under the U.S. Navy's pre-1962 designation system.
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Specifications
General Characteristics
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- Wingspan 27.6ft (8.4m)
- Length 43.7ft (13.3m)
- Height 18.4ft (5.6m)
- Empty Weight 10,586lbs (4,801kg)
- Loaded Weight 14,392lbs (6,528kg)
Performance
- Power/Weight Ratio 1.951
- Wing Loading 48.0lbs/ft2 (234.2kg/m2)
- Wing Area 300.1ft2 (27.9m2)
- Drag Points 3143
Parts
- Number of Parts 215
- Control Surfaces 7
- Performance Cost 933
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