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F-5F tiger II

399 LEMJ02industries  8.3 years ago
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The F-5F Tiger II is 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 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.After winning the International Fighter Aircraft competition in 1970, a program aimed at providing effective low-cost fighters to American allies, Northrop introduced the second-generation F-5E Tiger II in 1972. This upgrade included more powerful engines, higher fuel capacity, greater wing area and improved leading edge extensions for a better turn rate, optional air-to-air refueling, and improved avionics including air-to-air radar. Primarily used by American allies, it remains in US service to support training exercises. It has served in a wide array of roles, being able to perform both air and ground attack duties; the type was used extensively in Vietnam. A total of 1,400 Tiger IIs were built before production ended in 1987. More than 3,800 F-5 and T-38 aircraft were produced in Hawthorne, California.[4]The F-5 was also developed into a dedicated reconnaissance version, the RF-5 Tigereye. The F-5 also served as a starting point for a series of design studies which resulted in the Northrop YF-17 and the F/A-1

General Characteristics

  • Created On iOS
  • Wingspan 28.9ft (8.8m)
  • Length 32.6ft (9.9m)
  • Height 10.9ft (3.3m)
  • Empty Weight 2,921lbs (1,325kg)
  • Loaded Weight 6,890lbs (3,125kg)

Performance

  • Power/Weight Ratio 0.978
  • Wing Loading 44.0lbs/ft2 (214.6kg/m2)
  • Wing Area 156.7ft2 (14.6m2)
  • Drag Points 2069

Parts

  • Number of Parts 30
  • Control Surfaces 5
  • Performance Cost 196