Northrop F 5A/B
The Northrop F-5A/B Freedom Fighter and the F-5E/F Tiger II are part of asupersonic light fighter family, initially designed in the late 1950s by Northrop Corporation. Being smaller and simpler than contemporaries such as theMcDonnell 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. The F-5A entered service in the early 1960s. During the Cold War, over 800 were produced through 1972 for U.S. allies. Though the USAF had no acknowledged need for a light fighter, it did procure roughly 1,200 Northrop T-38 Talon trainer aircraft, which were directly based on the F-5A.
Specifications
General Characteristics
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- Wingspan 27.9ft (8.5m)
- Length 27.9ft (8.5m)
- Height 9.7ft (3.0m)
- Empty Weight 3,979lbs (1,805kg)
- Loaded Weight 6,066lbs (2,751kg)
Performance
- Power/Weight Ratio 1.111
- Wing Loading 43.3lbs/ft2 (211.5kg/m2)
- Wing Area 140.1ft2 (13.0m2)
- Drag Points 2100
Parts
- Number of Parts 74
- Control Surfaces 5
- Performance Cost 288