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