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      Lockheed YF-22 Raptor 
      
      
         
      
      In 1981 the Air Force developed a 
      requirement for an Advanced Tactical Fighter (ATF) as a new air 
      superiority fighter. It would take advantage of the new technologies in 
      fighter design on the horizon, including composite materials, lightweight 
      alloys, advanced flight control systems, higher power propulsion systems, 
      and stealth technology. Air Force leaders believed that these technologies 
      would make aircraft like the F-15 and F-16 obsolete by the early 21st 
      century. In 1985 the Air Force sent out formal requests for proposals to a 
      number of aircraft manufacturers and selected two industry teams, one led 
      by Lockheed, and the other by Northrop, to build the prototypes. The 
      Lockheed and Northrop teams each built two prototypes, one with General 
      Electric YF120 engines and one with Pratt & Whitney YF119 engines. The 
      Lockheed aircraft was designated YF-22 and the Northrop Aircraft was 
      YF-23. After extensive flight tests the Lockheed-Boeing-General Dynamics 
      team won the airframe competition and Pratt & Whitney the engine contract.
       
      SPECIFICATIONS
       
      Span: 43 ft. 0 in.  
      Length: 64 ft. 2 in.  
      Height: 17 ft. 9 in.  
      Armament: One M61 A2 20-millimeter cannon; internal stations can 
      carry AIM-9 Sidewinder infrared (heat seeking) air-to-air missiles and 
      AIM-120 AMRAAM radar-guided air-to-air missiles or 1,000-pound Joint 
      Direct Attack Munitions (JDAM) 
      Engines: Two Pratt & Whitney YF119-PW-100L engines. (The museum 
      aircraft originally flew with General Electric YF-120-GE-100 engines.) 
      Crew: One  
      PERFORMANCE
       
      Maximum speed: Mach 2+  
      Service Ceiling: Above 50,000 ft.  
      
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