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General Info

Vickers Limited
Wellington B Mark 1A

Role Medium bomber
anti-submarine aircraft
Manufacturer Vickers-Armstrongs
First flight 15 June 1936
Introduction October 1938
Retired March 1953
Primary users Royal Air Force
Royal Australian Air Force
Royal Canadian Air Force
Fleet Air Arm
Produced 1936–1945
Number built 11,461 or 11,462
Developed into Vickers Warwick
Vickers VC.1 Viking
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History Vickers Limited Armstrong Whitworth & Co Ltd
Wellington B Mark 1A the "Wimpey"



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, which was principally designed by Barnes Wallis. Development had been started in response to Air Ministry Specification B.9/32, issued in the middle of 1932, for a bomber for the Royal Air Force.

A larger heavy bomber aircraft designed to Specification B.1/35, the Vickers Warwick, was developed in parallel with the Wellington; the two aircraft shared around 85% of their structural components. Many elements of the Wellington were also re-used in a civil derivative, the Vickers VC.1 Viking.

Development

Wellingtons under construction, showing the geodetic airframe
RNZAF Wellington Mark I aircraft with the original turrets; anticipating war, the New Zealand government loaned these aircraft and their aircrews to the RAF in August 1939

In October 1932, the British Air Ministry invited Vickers to tender for the recently issued Specification B.9/32, which sought a twin-engine medium daylight bomber. In response, Vickers conducted a design study, led by Chief Designer Rex Pierson. Early on, Vickers' chief structures designer Barnes Wallis proposed the use of a geodetic airframe, inspired by his previous work on airships and the single-engined Wellesley light bomber. During structural testing performed at the Royal Aircraft Establishment, Farnborough, the proposed structure demonstrated not only the required strength factor of six, but reached 11 without any sign of failure, proving the geodetic airframe to possess a strength far in excess of normal levels. This strength allowed for the structure design to be further developed to reduce the size of individual members and adopt simplified standard sections of lighter construction..

National Airways Viscount at Wellington Airport, 1971
 

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Combat RANGE

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Vickers Limited Armstrong Whitworth & Co Ltd

Vickers Limited Armstrong Whitworth & Co Ltd
Vickers Wellington B Mark 1A

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General Info

      • Crew: five or six
      • Length: 64 ft 7 in (19.69 m)
      • Wingspan: 86 ft 2 in (26.26 m)
      • Height: 17 ft 5 in (5.31 m)
      • Wing area: 840 sq ft (78 m2)
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Powerplant


      • Empty weight: 18,556 lb (8,417 kg)
      • Max takeoff weight:  (12,927 kg)
      • Powerplant: 2 × Bristol Pegasus Mark XVIII radial engines, 1,050 hp (780 kW) each
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Performance

  • Maximum speed: 235 mph (378 km/h, 204 kn) at 15,500 ft (4,700 m)
  • Range: 2,550 mi (4,100 km, 2,220 nmi)
  • Service ceiling: 18,000 ft (5,500 m)
  • Rate of climb: 1,120 ft/min (5.7 m/s)
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Armament

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Special Links Vickers Limited Armstrong Whitworth & Co Ltd

Links to Youtube & Others

In late 1960, the People's Republic of China had begun negotiations with Vickers for as many as 40 Viscounts, but negotiations were protracted due to political tensions

Vickers Ltd.
Wellington B Mark 1A

BEA, and its nationalised successor British Airways (BA), vigorously operated the Viscount on Britain's domestic routes

interior

Youtube Link

The first airline in Latin America to operate the Viscount was Cubana de Aviación. Cubana's −755D Viscounts, delivered in 1956,

interior
Aircrafttotal : Aircraft

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