F-4 Phantom II vs Q-5 / A-5 Fantan
Overview
The F-4 Phantom II and the Q-5 / A-5 Fantan are both Combat Aircraft, manufactured by McDonnell and Nanchang respectively.
Top speed is 2,370 km/h for the F-4 Phantom II vs 1,210 km/h for the Q-5 / A-5 Fantan. The F-4 Phantom II has an operational range of 680 km vs 2,000 km for the Q-5 / A-5 Fantan. The F-4 Phantom II operates at altitudes up to 18,288 m compared to 16,500 m for the Q-5 / A-5 Fantan. At 28,030 kg MTOW, the F-4 Phantom II is 2.5x the Q-5 / A-5 Fantan's 11,300 kg.
The F-4 Phantom II has been produced in 5,195 units vs 1,300 for the Q-5 / A-5 Fantan. Unit cost is $3M for the F-4 Phantom II vs $1M for the Q-5 / A-5 Fantan. The F-4 Phantom II first flew 7 years before the Q-5 / A-5 Fantan (1958 vs 1965).
| 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 |
| Chinese ground-attack aircraft, notable for service in the Cold War period, often utilized in Pakistani and North Korean operations. | |
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| Origin country | π¨π³ China |
| Category | Combat Aircraft |
| Manufacturer | Nanchang |
| First flight | 4 June 1965 |
| Year introduced | 1970 |
| Number produced | 1300 units |
| Average unit price | $1 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 | 27.9 mΒ² β |
| Wingspan | 9.7 m β |
| Height | 4.3 m β |
| Length | 15.7 m β |
| Maximum speed | 1210 km/h β |
| Operational range | 2,000 km β |
| Service ceiling | 16,500 m β |
| Max. takeoff weight | 11,300 kg β |
| Empty weight | 6,400 kg β |
| Total thrust | 2 x 3,007 kgf β |
Performance Radar Chart
Detailed Comparison
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