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Vickers Wellington

6,232 Chingonito  6.5 years ago

The Vickers Wellington was a British twin-engined, long-range medium bomber. It was designed during the mid-1930s at Brooklands in Weybridge, Surrey, led by Vickers-Armstrongs' chief designer Rex Pierson; a key feature of the aircraft is its geodetic airframe fuselage structure, principally designed by Barnes Wallis. Development had been started in response to Air Ministry Specification B.9/32; issued in the middle of 1932, this called for a twin-engined day bomber capable of delivering higher performance than any previous design. Other aircraft developed to the same specification include the Armstrong Whitworth Whitley and the Handley Page Hampden. During the development process, performance requirements such as for the tare weight changed substantially, as well as the powerplant for the type being swapped.

General Characteristics

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  • Wingspan 34.2ft (10.4m)
  • Length 28.7ft (8.7m)
  • Height 12.0ft (3.7m)
  • Empty Weight 5,897lbs (2,674kg)
  • Loaded Weight 6,761lbs (3,066kg)

Performance

  • Horse Power/Weight Ratio 0.443
  • Wing Loading 34.7lbs/ft2 (169.6kg/m2)
  • Wing Area 194.6ft2 (18.1m2)
  • Drag Points 2446

Parts

  • Number of Parts 45
  • Control Surfaces 5
  • Performance Cost 305