F-16XL Fighting Falcon
| Specifications | ||
|---|---|---|
| Crew size |
F-16XL-2 two-seat cockpit F-16XL-1 single-seat aircraft | |
| Length | 54.2 ft (16.52 m) | |
| Wingspan | 34.3 ft (10.45 m) | |
| height at vertical tail | 17.7 ft (5.39 m). | |
| Max. weight | 48,000 lb (17,915.60 kg) | |
| Engines |
| |
| Controls | Both aircraft featured an analog fly-by-wire electronic flight control system during the laminar flow research. The single-seat aircraft now has a digital flight control system. | |
| Wing construction | The delta (cranked arrow) wings on both aircraft are manufactured of advanced graphite composites to provide strength for high wing loads during flight. | |
| Design load | Baseline F-16XL: 9 "Gs". Modified F-16XL: 3 "Gs") | |
| Maximum Speed |
F-16XL-2, Mach 2 (approx. 1,400 mph) (2,253 k/hr) F-16XL-1, Mach 1.8 (approx. 1,260 mph) | |
| Range | Over 2,500 nautical miles (4,630 k), without in-flight refueling, and unlimited with in-flight refueling | |
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