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      Lockheed F-94C Starfire 
      
      
       
      The F-94 series all-weather interceptors 
      were developed from the Lockheed F-80 Shooting Star. The prototype F-94 
      first flew on July 1, 1949. The Starfire was subsequently produced in the 
      -A, -B, and -C series. The F-94C (originally designated the F-97A) was a 
      fundamental redesign of the F-94B and made its first flight on January 18, 
      1950.  
      Improvements in the F-94C included a 
      higher thrust engine, single point refuelling, a redesigned wing, a 
      sweptback horizontal stabilizer, upgraded fire-control and navigation 
      systems and, later, mid-wing rocket pods. Twenty-four rockets were carried 
      in the nose in a ring around the radome, shielded by retractable doors, 
      with an additional 24 in the wing pods, if installed. The F-94C carried no 
      guns. Starfires were employed in the air defence of the Continental U.S. 
      in the 1950s. In the F-94A form, they served as the first all-jet 
      all-weather interceptor for the Air Defence Command. The last F-94Cs were 
      withdrawn from USAF service in 1959.  
      SPECIFICATIONS
       
      Span: 37 ft. 4 in.  
      Length: 44 ft. 6 in.  
      Height: 14 ft. 11 in.  
      Weight: 24,000 lbs. loaded  
      Armament: Twenty-four 2.75 in. Folding Fin Air Rockets (FFARs) in 
      nose and twenty-four FFARs in two wing pods  
      Engine: Pratt & Whitney J48-P-5 or -5A of 8,750 lbs. thrust with 
      afterburner  
      Crew: Two  
      Cost: $534,000  
      Serial Number: 50-980  
      C/N: 880-8025  
      Displayed As:50-1054  
      PERFORMANCE
       
      Maximum speed: 640 mph.  
      Cruising speed: 476 mph.  
      Range: 1,275 miles 
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