Northrup Grumman F-5E Tiger II
The Northrop F-5A and F-5B Freedom Fighter and the F-5E and F-5F 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. 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 United States Air Force (USAF) had no acknowledged need for a light fighter, it did procure approximately 1,200 Northrop T-38 Talon trainer aircraft, which were directly based on the F-5A.
Specifications
General Characteristics
- Predecessor Grumman F-9F Cougar
- Successors 1 airplane(s)
- Created On iOS
- Wingspan 24.0ft (7.3m)
- Length 35.1ft (10.7m)
- Height 12.3ft (3.7m)
- Empty Weight 10,148lbs (4,603kg)
- Loaded Weight 13,297lbs (6,031kg)
Performance
- Power/Weight Ratio 1.69
- Wing Loading 67.7lbs/ft2 (330.8kg/m2)
- Wing Area 196.3ft2 (18.2m2)
- Drag Points 1837
Parts
- Number of Parts 55
- Control Surfaces 5
- Performance Cost 297