Armstrong Whitworth A.W.52

From Wikipedia, the free encyclopedia

Armstrong Whitworth A.W.52
Type 3/4 scale experimental aircraft
Manufacturer Armstrong Whitworth
Designed by John Lloyd
Maiden flight 13 November 1947
Primary user UK
Number built 2


The A.W.52 was a British flying wing aircraft design of the late 1940s built by Armstrong Whitworth.

Contents

[edit] History

Armstrong Whitworth proposed a jet-powered four engine flying wing design during the Second World War. This would utilitise a laminar flow wing.

The design was tested on a third-scale glider known as the A.W.52G but the war ended and the bomber project was dropped but received a contract that would allow them to produce two prototypes for evaluation nominally for a mail carrying aircraft. The first prototype flew on 13 November 1947 powered by two Rolls Royce Nene engines. This was followed by the second on 1 September 1948 with the Rolls Royce Derwent. The first prototype crashed without loss of life in May 1949, making it the first occasion of an emergency ejection by a British pilot, but the second prototype remained flying with the Royal Aircraft Establishment until 1954.

[edit] Specification

[edit] Dimensions

  • Crew : 2
  • Wing Span: 90 ft
  • Length: 37 ft 4 in.
  • Height: 14 ft 4 in.
  • Weight:
Empty: 19,662 lb
Laden: 34,154 lb
  • Powerplant: two Rolls Royce Nene turbojets (5,000 lbf each)

[edit] Performance

  • Maximum Speed: 500 mph
  • Ceiling: 36,000 ft
  • Range: 980 miles

[edit] External links

[edit] See also

Related development: None

Comparable aircraft:

Designation series: A.W.27 - A.W.38 - A.W.41 - A.W.52 - A.W.55


United Kingdom military stub This United Kingdom military article is a stub. You can help Wikipedia by expanding it.