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.
Specifications
Spotlights
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General Characteristics
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- Wingspan 34.1ft (10.4m)
- Length 48.0ft (14.6m)
- Height 20.5ft (6.2m)
- Empty Weight 16,624lbs (7,540kg)
- Loaded Weight 29,249lbs (13,267kg)
Performance
- Power/Weight Ratio 3.226
- Wing Loading 67.0lbs/ft2 (327.1kg/m2)
- Wing Area 436.6ft2 (40.6m2)
- Drag Points 6047
Parts
- Number of Parts 179
- Control Surfaces 5
- Performance Cost 854
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