F-16 Fighting Falcon vs SO 4050 Vautour
Overview
The F-16 Fighting Falcon and the SO 4050 Vautour are both Combat Aircraft, manufactured by General Dynamics and Sud Aviation respectively.
The F-16 Fighting Falcon reaches 2,410 km/h β 2.2x the SO 4050 Vautour's 1,106 km/h. The F-16 Fighting Falcon has an operational range of 546 km vs 1,200 km for the SO 4050 Vautour. The F-16 Fighting Falcon operates at altitudes up to 18,288 m compared to 15,200 m for the SO 4050 Vautour.
The F-16 Fighting Falcon has been produced in 4,604 units vs 149 for the SO 4050 Vautour. Unit cost is $75M for the F-16 Fighting Falcon vs $2M for the SO 4050 Vautour. The SO 4050 Vautour first flew 22 years before the F-16 Fighting Falcon (1952 vs 1974).
| American multirole fighter, famed in late Cold War conflicts, renowned for performance in precision daytime strikes and defensive counter air operations. | |
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| Origin country | πΊπΈ United States |
| Category | Combat Aircraft |
| Manufacturer | General Dynamics |
| First flight | 2 February 1974 |
| Year introduced | 1979 |
| Number produced | 4604 units |
| Average unit price | $75 million |
| French jet-powered multirole aircraft, developed in the 1950s, utilized in combat operations during the Six-Day War by Israel. | |
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| Origin country | π«π· France |
| Category | Combat Aircraft |
| Manufacturer | Sud Aviation |
| First flight | 16 October 1952 |
| Year introduced | 1956 |
| Number produced | 149 units |
| Average unit price | $2 million |
| Wing area | 27.9 mΒ² β |
| Wingspan | 10.0 m β |
| Height | 4.9 m β |
| Length | 15.1 m β |
| Maximum speed | 2410 km/h β |
| Operational range | 546 km β |
| Service ceiling | 18,288 m β |
| Max. takeoff weight | 19,200 kg β |
| Empty weight | 8,570 kg β |
| Total thrust | 1 x 7,777 kgf β |
| Wing area | 45.0 mΒ² β |
| Wingspan | 15.1 m β |
| Height | 4.9 m β |
| Length | 15.6 m β |
| Maximum speed | 1106 km/h β |
| Operational range | 1,200 km β |
| Service ceiling | 15,200 m β |
| Max. takeoff weight | 21,000 kg β |
| Empty weight | 10,000 kg β |
| Total thrust | 2 x 3,700 kgf β |
Performance Radar Chart
Detailed Comparison
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