F-4 Phantom II vs IAR-93 / J-22 Orao
Overview
The F-4 Phantom II and the IAR-93 / J-22 Orao are both Combat Aircraft, manufactured by McDonnell and CNIAR/Soko respectively.
The F-4 Phantom II reaches 2,370 km/h β 2.2x the IAR-93 / J-22 Orao's 1,094 km/h. The F-4 Phantom II has an operational range of 680 km vs 1,320 km for the IAR-93 / J-22 Orao. The F-4 Phantom II operates at altitudes up to 18,288 m compared to 13,600 m for the IAR-93 / J-22 Orao. At 28,030 kg MTOW, the F-4 Phantom II is 2.6x the IAR-93 / J-22 Orao's 10,900 kg.
The F-4 Phantom II has been produced in 5,195 units vs 88 for the IAR-93 / J-22 Orao. Unit cost is $3M for the F-4 Phantom II vs $10M for the IAR-93 / J-22 Orao. The F-4 Phantom II first flew 16 years before the IAR-93 / J-22 Orao (1958 vs 1974).
| 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 |
| Romanian-Yugoslav ground-attack aircraft, operational during the Cold War, used significantly in the Yugoslav Wars. | |
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| Origin country | π·π΄ Romania π³π± Ex-Yugoslavia |
| Category | Combat Aircraft |
| Manufacturer | CNIAR/Soko |
| First flight | 31 August 1974 |
| Year introduced | 1977 |
| Number produced | 88 units |
| Average unit price | $10 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 | 26.0 mΒ² β |
| Wingspan | 9.3 m β |
| Height | 4.5 m β |
| Length | 14.9 m β |
| Maximum speed | 1094 km/h β |
| Operational range | 1,320 km β |
| Service ceiling | 13,600 m β |
| Max. takeoff weight | 10,900 kg β |
| Empty weight | 5,750 kg β |
| Total thrust | 2 x 1,814 kgf β |
Performance Radar Chart
Detailed Comparison
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