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The Lockheed/ Boeing/ General Dynamics YF-22 is an American single-seat, twin-engine, stealth fighter technology demonstrator prototype designed for the United States Air Force (USAF). The design team, with Lockheed as the prime contractor, was a finalist in the USAF's Advanced Tactical Fighter (ATF) competition, and two prototypes were built ...
Lockheed YF-22. I have added considerable amount of design history information compiled from several sources to give a summary of how the design came to be. I believe this article can be considered for A-class. Steve7c8 14:35, 9 July 2024 (UTC)
A YF-22 in the foreground with a YF-23 in the background The two contractor teams submitted evaluation results and their PSC proposals for full-scale development in December 1990, [ 57 ] and on 23 April 1991, Donald Rice , the Secretary of the Air Force announced that the YF-22 team was the winner. [ 71 ]
A MIL-DTL-38999 circular connector plated with a nickel–teflon composite. Left: plug (male) type connector; Right: receptacle (female) type connector) Electrical or fiber-optic connectors used by U.S. Department of Defense were originally developed in the 1930s for severe aeronautical and tactical service applications, and the Type "AN" series set the standard for modern military circular ...
The YF120-powered the YF-22 and YF-23 to supercruise speeds of Mach 1.58 and Mach 1.72 respectively. [6] [7] [N 1] The first YF-22 (right), registration number N22YF, was powered by two YF120 engines. The Engineering & Manufacturing Development (EMD) configuration of the F120 was tested in December 1990.
Lockheed YF-22; Mikoyan Project 1.44; Northrop Grumman B-2 Spirit; Northrop YF-23 (inverse S-duct) Short SC.1; Sukhoi Su-47; Tupolev Tu-154; Tupolev Tu-154M; Yakovlev Yak-40; Yakovlev Yak-42; The Boeing 747-300 Trijet (not to be confused with the later 747-300) was designed with an S-duct layout, but never built.