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Global Aircraft -- F-16XL
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F-16XL
Specifications
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Achievements
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Features
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Photos
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F-16XL Specifications
Primary Function:
experimental - Laminar Flow Research Aircraft
Contractor:
General Dynamics Corp.
Crew:
One
Unit Cost:
N/A
Powerplant
Pratt and Whitney 100-PW-100 engine (with afterburner), rated at 23,830 lb thrust
Dimensions
Length:
54.2 ft (16.52 m)
Wingspan:
34.3 ft (10.45 m)
Height:
17.7 ft (5.39 m)
Weights
Empty:
N/A
Max. Weight:
48,000 lb (17,915.60 kg)
Performance
Speed:
Mach 1.8 (1,260 mph)
Ceiling:
50,000 ft
Range:
2,850 miles
Armament
N/A
F-16XL
(Ship #2)
Specifications
Primary Function:
experimental - Laminar Flow Research Aircraft
Contractor:
General Dynamics Corp.
Crew:
Two
Unit Cost:
N/A
Powerplant
General Electric F110-GE-129 engine (with afterburner) rated at 29,000 lb thrust
Dimensions
Length:
54.2 ft (16.52 m)
Wingspan:
34.3 ft (10.45 m)
Height:
17.7 ft (5.39 m)
Weights
Empty:
N/A
Max. Weight:
48,000 lb (17,915.60 kg)
Performance
Speed:
Mach 2 (1,400 mph)
Ceiling:
50,000 ft
Range:
2,850 miles
Armament
N/A
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F-16XL Achievements
The F-16XL was the first program to look at laminar flow on swept wings at speeds representative of those at which a high speed civil transport might fly.
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F-16XL Features
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F-16XL Background
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F-16XL Photos
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