uncited changes and in the wrong place (i.e. a list of preserved aircraft)
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The '''Northrop F-5''' is a family of [[supersonic]] [[light fighter]] aircraft initially designed as a privately funded project in the late 1950s by [[Northrop Corporation]]. There are two main models, the original '''F-5A''' and '''F-5B Freedom Fighter''' variants and the extensively updated '''F-5E''' and '''F-5F Tiger II''' variants. The design team wrapped a small, highly aerodynamic fighter around two compact and high-thrust [[General Electric J85]] engines, focusing on performance and a low cost of maintenance. Smaller and simpler than contemporaries such as the [[McDonnell Douglas F-4 Phantom II]], the F-5 cost less to procure and operate, making it a popular export aircraft. Though primarily designed for a 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 US allies. Though at the time the [[United States Air Force]] (USAF) did not
After winning the International Fighter Aircraft Competition, a program aimed at providing effective low-cost fighters to American allies, in 1972 Northrop introduced the second-generation F-5E Tiger II. This upgrade included more powerful engines, larger fuel capacity, greater wing area and improved leading edge extensions for better turn rates, optional air-to-air
The F-5 was also developed into a dedicated [[reconnaissance aircraft]], 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-18 Hornet|F/A-18]] naval fighter aircraft. The [[Northrop F-20 Tigershark]] was an advanced variant to succeed the F-5E which was ultimately
==Design and development==
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The design effort was led by Northrop vice president of engineering and aircraft designer [[Edgar Schmued]],<ref>{{harvnb|Garrison|2005}}</ref> who previously at [[North American Aviation]] had been the chief designer of the successful [[North American P-51 Mustang]] and [[North American F-86 Sabre|F-86 Sabre]] fighters. Schmued recruited a strong engineering team to Northrop.<ref>{{harvnb|Wagner|2000|p=195}}.</ref>
In December 1953, [[NATO]] issued [[NBMR-1]], calling for a lightweight tactical fighter capable of carrying conventional and nuclear weapons and operating from rough airfields. In late 1954, a Northrop team toured Europe and Asia to examine both the NBMR-1 and the needs of [[SEATO]] members. From this tour, Schmued gave his team the goal of reversing the trend in fighter development towards greater size and weight
The design began to firm up in 1955 with the introduction of the [[General Electric J85]] turbojet engine. Originally developed for McDonnell's [[ADM-20 Quail]] decoy for use on the [[Boeing B-52 Stratofortress]],<ref name="Claws p111-4">{{harvnb|Braybrook|1982|pp=111–114}}.</ref> the J85 had a [[thrust-to-weight ratio]] of 6.25 to 7.5 depending on the version, giving it a notable advantage over contemporaries such as the 4.7 ratio of the [[J79]] engine used in the [[McDonnell Douglas F-4 Phantom II|F-4 Phantom]].<ref>{{harvnb|Stuart|1978|p=21}}.</ref>
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