The Lockheed F-104 Starfighter is an American single-engine, supersonic air superiority fighter which was extensively deployed as a fighter-bomber during the Cold War. Created as a day fighter by Lockheed as one of the "Century Series" of fighter aircraft for the United States Air Force (USAF), it was developed into an all-weather multirole aircraft in the early 1960s and produced by several other nations, seeing widespread service outside the United States.
After a series of interviews with Korean War fighter pilots in 1951, Kelly Johnson, then lead designer at Lockheed, opted to reverse the trend of ever-larger and more complex fighters to produce a simple, lightweight aircraft with maximum altitude and climb performance. On 4 March 1954, the Lockheed XF-104 took to the skies for the first time, and on 26 February 1958, the production fighter was activated by the USAF. Just a few months later, it was pressed into action during the Second Taiwan Strait Crisis, when it was deployed as a deterrent to Chinese MiG-15 and MiG-17 fighters. Problems with the General Electric J79 engine and a preference for fighters with longer ranges and heavier payloads meant its service with the USAF was short-lived, though it was reactivated for service during the Berlin Crisis of 1961 and the Vietnam War, when it flew more than 5,000 combat sorties.
While its time with the USAF was brief, the Starfighter found much more lasting success with other NATO and allied nations. In October 1958, West Germany selected the F-104 as its primary fighter aircraft. Canada soon followed, along with the Netherlands, Belgium, Japan, and Italy. The European nations formed a construction consortium that was the largest international manufacturing program in history to that point, though the Starfighter's export success was marred in 1975 by the discovery of bribe payments made by Lockheed to many foreign military and political figures for securing purchase contracts.
Specifications
Spotlights
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General Characteristics
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- Wingspan 25.5ft (7.8m)
- Length 55.1ft (16.8m)
- Height 13.7ft (4.2m)
- Empty Weight 13,563lbs (6,152kg)
- Loaded Weight 14,885lbs (6,752kg)
Performance
- Power/Weight Ratio 2.264
- Wing Loading 59.5lbs/ft2 (290.4kg/m2)
- Wing Area 250.3ft2 (23.3m2)
- Drag Points 3437
Parts
- Number of Parts 64
- Control Surfaces 8
- Performance Cost 320