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The Lockheed F-104 Starfighter is an American single-engine, supersonic interceptor 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 ...
The aircraft is a single place, single engine gull-wing design with retractable conventional landing gear. The F4U was the second completed aircraft in the W.A.R. series, with the first example displayed at the EAA airshow in 1975. The aircraft featured folding wings. [3]
Development of the company's first design, the W.A.R. Focke-Wulf 190, commenced in 1973, with the first flight following in 1974.The aircraft are all half-scale World War II fighter aircraft replicas, based on a common design, consisting of a wooden fuselage box shape and wooden spar wing.
The first YF-93 in flight. The prototypes, serial numbers 48-317 and -318, began flight tests in 1950 and were entered in a flyoff against the other penetration fighter projects, the XF-88 and XF-90; the XF-88 Voodoo was declared the winner. None of the projects would be ordered.
NASA HGU-26P helmet for the Northrop T-38 Talon aircraft German leather flight helmet of World War I. A flight helmet, sometimes referred to as a "skull dome", "bone dome" or "foam dome", is a special type of helmet primarily worn by military aircrew. A flight helmet can provide: [1]
Clarence L. "Kelly" Johnson, chief engineer at Lockheed's Skunk Works, visited Korea in December 1951 and talked to fighter pilots about what sort of aircraft they wanted. . At the time, U.S. Air Force pilots were confronting the MiG-15 "Fagot" in their North American F-86 Sabres, and many of the pilots felt that the MiGs were superior to the larger and more complex American desi
The Lockheed NF-104A is an American mixed-power, high-performance, supersonic aerospace trainer that served as a low-cost astronaut training vehicle for the North American X-15 and projected Boeing X-20 Dyna-Soar programs.
Only a limited fuel supply of 112 US gal (93 imp gal; 420 L) was deemed necessary for the specified 30-minute combat endurance. [10] A hook was installed along the aircraft's center of gravity; in flight, it retracted to lie flat in the upper part of the nose. [10] The aircraft had an empty weight just short of 4,000 pounds (1.8 t). [11]