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      Avro Vulcan 
      
        
      A post-WWII analysis of 
      Allied strategic bombing affirmed the success of such tactics during the 
      war. The new importance of nuclear weapons made it all the more imperative 
      that the world's nuclear powers have long-range delivery capabilities. 
      England's Royal Air Force (RAF) issued a requirement for a new aircraft 
      design which could be based anywhere in the world, be able to strike 
      targets up to 1,700 miles away, and deliver a heavy bomb load from high 
      speed and high altitude. One of the three finalists for the job was the 
      Avro Vulcan, first flown on 3 August 1952. The Vulcan's main distinctive 
      physical characteristic, its large delta-wing shape, was a result of the 
      need for structural integrity and a large payload capacity. To prove the 
      as-yet untested design, the Avro company built a series of one-third scale 
      aircraft, designated as Avro 707s. 
      The 
      first production model of the Vulcan, the B.Mk 1, 
      flew in early 1955, and after a few airframe and wing design changes, 
      entered service. While the first prototype Vulcans were powered by four 
      6,500-pound thrust Rolls-Royce Avon RA.3 engines, a series of engine 
      upgrades throughout its lifetime resulted in a final configuration of four 
      20,000-pound thrust Rolls-Royce Olympus 301s, giving the Vulcan 
      significant performance improvements over earlier marks. 
      
      Numerous other design improvements were gradually incorporated as well, as 
      follows: The B.Mk 1A variant incorporated a 
      modified tailcone housing an Electronic Counter-Measures (ECM) system. The
      B.Mk 2 had more powerful engines than the B.Mk 
      1, a much-modified and larger wing, elevons for pitch and roll control 
      (instead of separate elevators and ailerons), an auxiliary power unit (APU), 
      in-flight refueling capability, and modified weapons-launch capability. In 
      the mid 1960s the B.Mk 2 was adapted as a long-range, low-level 
      conventional bomber. Finally, the SR.Mk 2 
      strategic reconnaissance variant appeared in 1973. 
      The 
      Vulcan remained on active duty with the RAF into the 1980s. Few retired 
      aircraft types retain the mystique enjoyed by the handful of remaining 
      examples of the Vulcan which have found their way into museums. For almost 
      a decade after its retirement, at least one Vulcan was flown at air 
      displays throughout Europe and the British Isles, but financial 
      considerations resulted in all Vulcans being grounded by the mid 1990s. 
      
      Nicknames:
      Iron Overcast; The Tin Triangle 
      
      Specifications (B.Mk 2): 
      
              Engines: Four 20,000-pound thrust 
      Rolls-Royce Olympus 301 turbojets  
              Max Takeoff Weight: ~250,000 lbs. 
              Wing Span: 111ft. 0in. 
              Length: 99ft. 11in. 
              Height: 27ft. 2in. 
              Performance: 
                  Maximum Speed: 645 mph 
                  Ceiling: 65,000 ft. 
                  Range: 4,600 miles with normal bomb-load 
              Armament: Up to 21,000 pounds of bombs, carried internally 
      
      Number Built: 
      134 
      
      Number Still Airworthy: 
      None  |