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McDonnell Douglas F-15C Eagle
Military
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Northrop Corporation F-5E Tiger II
Military
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|---|---|---|
| Quick facts | ||
| Manufacturer | McDonnell Douglas | Northrop Corporation |
| Type | Fighters & multirole | Fighters & multirole |
| Origin | 🇺🇸 United States | 🇺🇸 United States |
| First flight | 1972 | 1972 |
| Status | In service | In service |
| Units built | — | 1,400 |
| Unit cost | — | — |
| Dimensions | ||
| Length | 19.43 m | 14.45 m |
| Wingspan | 13.05 m | 8.13 m |
| Height | 5.63 m | 4.08 m |
| Wing area | 56.5 m² | 17.3 m² |
| Weights & fuel | ||
| Empty weight | 12,700 kg | 4,349 kg |
| Max. take-off weight | 30,845 kg | 11,187 kg |
| Performance | ||
| Max. speed | 2,655 km/h | 1,700 km/h |
| Max. Mach | Mach 2.50 | Mach 1.60 |
| Range | — | 1,405 km |
| Ferry range | 5,550 km | — |
| Combat radius | 1,967 km | — |
| Service ceiling | 20,000 m | 15,800 m |
| Rate of climb | 254.0 m/s | 175.0 m/s |
| Crew & capacity | ||
| Crew | 1 | 1 |
| Hardpoints | — | 7 |
| Powerplant | ||
| Engines | 2 | 2 |
| Engine type | — | — |
| Engine model | Pratt & Whitney F100-PW-220 | GE J85-GE-21 |
| Thrust (each) | 64.9 kN | 15.5 kN |
| Thrust with afterburner (each) | 105.7 kN | 22.2 kN |
At a glance
Figures are compiled from public sources and may be approximate; they can vary by variant and configuration.