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Lockheed Martin F-16 Fighting Falcon
Military
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Mitsubishi Heavy Industries F-2
Military
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|---|---|---|
| Quick facts | ||
| Manufacturer | Lockheed Martin | Mitsubishi Heavy Industries |
| Type | Fighters & multirole | Fighters & multirole |
| Origin | 🇺🇸 United States | 🇯🇵 Japan |
| First flight | 1974 | 1995 |
| Status | In production | In service |
| Units built | 4,600 | 98 |
| Unit cost | — | — |
| Dimensions | ||
| Length | 15.06 m | 15.52 m |
| Wingspan | 9.96 m | 11.13 m |
| Height | 4.88 m | 4.96 m |
| Wing area | 27.9 m² | 34.8 m² |
| Weights & fuel | ||
| Empty weight | 8,570 kg | 9,527 kg |
| Max. take-off weight | 19,187 kg | 22,100 kg |
| Performance | ||
| Max. speed | 2,120 km/h | — |
| Max. Mach | Mach 2.05 | Mach 2.00 |
| Ferry range | 4,220 km | — |
| Combat radius | 550 km | 830 km |
| Service ceiling | 15,240 m | 18,000 m |
| Rate of climb | 254.0 m/s | — |
| Crew & capacity | ||
| Crew | 1–2 | 1–2 |
| Hardpoints | 11 | 11 |
| Powerplant | ||
| Engines | 1 | 1 |
| Engine type | — | — |
| Engine model | GE F110-GE-129 or P&W F100-PW-229 | GE F110-GE-129 |
| Thrust (each) | 76.3 kN | 76.3 kN |
| Thrust with afterburner (each) | 131.0 kN | 131.0 kN |
At a glance
Figures are compiled from public sources and may be approximate; they can vary by variant and configuration.