The Douglas A-4 Skyhawk is a single seat subsonic carrier-capable 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
General Characteristics
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- Wingspan 21.4ft (6.5m)
- Length 29.0ft (8.8m)
- Height 15.1ft (4.6m)
- Empty Weight 6,610lbs (2,998kg)
- Loaded Weight 10,418lbs (4,725kg)
Performance
- Power/Weight Ratio 1.078
- Wing Loading 53.8lbs/ft2 (262.5kg/m2)
- Wing Area 193.8ft2 (18.0m2)
- Drag Points 1974
Parts
- Number of Parts 53
- Control Surfaces 5
- Performance Cost 260
