A-4 Skyhawk vs F-8 Crusader
| American light attack jet, extensively deployed in the Vietnam War, notable for carrier-based operations and close air support roles. | |
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| Origin country | 🇺🇸 United States |
| Category | Combat Aircraft |
| Manufacturer | McDonnell Douglas |
| First flight | 22 June 1954 |
| Year introduced | 1956 |
| Number produced | 2960 units |
| Average unit price | $2 million |
| American fighter aircraft, notable for its Cold War-era use, largely deployed in the Vietnam War and the Cuban Missile Crisis. | |
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| Origin country | 🇺🇸 United States |
| Category | Combat Aircraft |
| Manufacturer | Vought |
| First flight | 25 March 1955 |
| Year introduced | 1957 |
| Number produced | 1219 units |
| Average unit price | $2.5 million |
| Wing area | 24.2 m² ◉ |
| Wingspan | 8.4 m â—‰ |
| Height | 4.6 m â—‰ |
| Length | 12.2 m â—‰ |
| Maximum speed | 1077 km/h â—‰ |
| Operational range | 3,300 km â—‰ |
| Service ceiling | 12,880 m â—‰ |
| Max. takeoff weight | 11,136 kg â—‰ |
| Empty weight | 4,750 kg â—‰ |
| Total thrust | 1 x 4,100 kgf â—‰ |
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| Wing area | 34.8 m² ◉ |
| Wingspan | 10.9 m â—‰ |
| Height | 4.8 m â—‰ |
| Length | 16.5 m â—‰ |
| Maximum speed | 1971 km/h â—‰ |
| Operational range | 730 km â—‰ |
| Service ceiling | 17,678 m â—‰ |
| Max. takeoff weight | 13,000 kg â—‰ |
| Empty weight | 7,956 kg â—‰ |
| Total thrust | 1 x 4,853 kgf â—‰ |
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Performance Radar Chart
Photo of A-4 Skyhawk by US Marine Corps.