F-4 Phantom II vs Mirage III / 5 / 50
Overview
The F-4 Phantom II and the Mirage III / 5 / 50 are both Combat Aircraft, manufactured by McDonnell and Dassault respectively.
Top speed is 2,370 km/h for the F-4 Phantom II vs 2,350 km/h for the Mirage III / 5 / 50. The F-4 Phantom II has an operational range of 680 km vs 2,400 km for the Mirage III / 5 / 50. The F-4 Phantom II operates at altitudes up to 18,288 m compared to 17,000 m for the Mirage III / 5 / 50. At 28,030 kg MTOW, the F-4 Phantom II is 2.3x the Mirage III / 5 / 50's 12,000 kg.
The F-4 Phantom II has been produced in 5,195 units vs 1,422 for the Mirage III / 5 / 50. Unit cost is $3M for the F-4 Phantom II vs $5M for the Mirage III / 5 / 50. The Mirage III / 5 / 50 first flew 2 years before the F-4 Phantom II (1956 vs 1958).
| American fighter-bomber, renowned for its widespread use in the Vietnam War and numerous other international military conflicts. | |
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| Origin country | πΊπΈ United States |
| Category | Combat Aircraft |
| Manufacturer | McDonnell |
| First flight | 27 May 1958 |
| Year introduced | 1962 |
| Number produced | 5195 units |
| Average unit price | $3 million |
| French jet fighter-bomber, notable for its role in multiple conflicts globally since the 1960s, including the Six-Day War. | |
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| Origin country | π«π· France |
| Category | Combat Aircraft |
| Manufacturer | Dassault |
| First flight | 17 November 1956 |
| Year introduced | 1961 |
| Number produced | 1422 units |
| Average unit price | $5 million |
| Wing area | 49.2 mΒ² β |
| Wingspan | 11.7 m β |
| Height | 5.0 m β |
| Length | 19.0 m β |
| Maximum speed | 2370 km/h β |
| Operational range | 680 km β |
| Service ceiling | 18,288 m β |
| Max. takeoff weight | 28,030 kg β |
| Empty weight | 13,757 kg β |
| Total thrust | 2 x 8,093 kgf β |
| Wing area | 34.8 mΒ² β |
| Wingspan | 8.2 m β |
| Height | 4.5 m β |
| Length | 15.3 m β |
| Maximum speed | 2350 km/h β |
| Operational range | 2,400 km β |
| Service ceiling | 17,000 m β |
| Max. takeoff weight | 12,000 kg β |
| Empty weight | 6,740 kg β |
| Total thrust | 1 x 4,300 kgf β |
Performance Radar Chart
Detailed Comparison
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