F5E-Tiger II MK4
The Northrop F-5A/B Freedom Fighter and the F-5E/F Tiger II are part of a supersonic light fighter family, initially designed in the late 1950s by Northrop Corporation. Being smaller and simpler than contemporaries such as the McDonnell Douglas F-4 Phantom II, the F-5 cost less to both procure and operate, making it a popular export aircraft. The F-5 started life as a privately funded light fighter program by Northrop in the 1950s. The design team wrapped a small, highly aerodynamic fighter around two compact and high-thrust General Electric J85 engines, focusing on performance and low cost of maintenance. Though primarily designed for the day air superiority role, the aircraft is also a capable ground-attack platform. From Wikipedia
Specifications
General Characteristics
- Predecessor F-5E Tiger shark
- Successors 1 airplane(s)
- Created On iOS
- Wingspan 19.4ft (5.9m)
- Length 25.4ft (7.8m)
- Height 7.3ft (2.2m)
- Empty Weight 3,014lbs (1,367kg)
- Loaded Weight 3,787lbs (1,717kg)
Performance
- Power/Weight Ratio 1.78
- Wing Loading 29.1lbs/ft2 (142.3kg/m2)
- Wing Area 130.0ft2 (12.1m2)
- Drag Points 1396
Parts
- Number of Parts 37
- Control Surfaces 5
- Performance Cost 225
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