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Miles M.20 - Wikipedia, the free encyclopedia

Miles M.20

From Wikipedia, the free encyclopedia

M.20

Second prototype of the Miles M.20

Type Lightweight fighter
Manufacturer Miles Aircraft
Maiden flight 15 September 1940
Introduced Cancelled
Primary users Royal Air Force (intended)
Fleet Air Arm (intended)
Number built 2 prototypes
Developed from Miles Master

The Miles M.20 was a Second World War fighter developed by Miles Aircraft in 1940. Designed and built as a simple and cheap alternative to the Royal Air Force Spitfire and Hurricane, its design was overtaken by events.

Contents

[edit] Design and development

During the Battle of Britain, the Royal Air Force was faced with a potential shortage of fighters. To meet the Luftwaffe threat, the Air Ministry commissioned Miles to design the M.20; nine weeks and two days later the first prototype flew.[1]

To reduce production times the M.20 was of an all-wood construction, used many parts from the earlier Miles Master trainer, lacked hydraulics, and had streamlined fixed landing gear. The engine was a complete Rolls-Royce Merlin XX "power egg", and was identical to those used on the Avro Lancaster and some Bristol Beaufighter marks. The design also featured a bubble canopy for improved pilot visibility, one of the first fighters to do so.

[edit] Testing and evaluation

The first prototype, with the serial U-9 first flew 15 September 1940 and tested at the A & AEE as AX834 in compliance with Specification F.19/40. Armed with the same eight .303 Browning machine guns as the Hawker Hurricane, the M.20 prototype was faster than the Hurricane and slower than the Spitfire types then in production, but carried more ammunition, and had greater range than either. As the Luftwaffe was defeated over Britain, the need for the M.20 vanished and the design was abandoned without entering production. The first prototype was later scrapped at Woodley.

A second prototype, U-0228 and later serialed as DR616, was built to Specification N.1/41 for a Fleet Air Arm shipboard fighter, equipped with an arrestor hook and catapult launch points. It first flew on 8 April 1941. This variant was also fitted with jettisonable undercarriage so it could be used from catapults on CAM ships (Catapult Aircraft Merchantmen), however these ships had no flight decks so the aircraft had to be ditched into the sea after just one mission. Old and tired Hawker Hurricanes took on this role, relegating the M.20 as superfluous and consequently leading to the scrapping of the shipboard variant.

[edit] Specifications (M.20, as tested)

Data from British Aircraft of World War II[2] and Military.cz[3]

General characteristics

  • Crew: One pilot
  • Length: 30 ft 8 in (9.35 m)
  • Wingspan: 34 ft 7 in (10.54 m)
  • Height: 12 ft 6 in (3.81 m)
  • Wing area: 234 ft² (21.74 m²)
  • Empty weight: 5,870 lb (2,663 kg)
  • Max takeoff weight: 8,000 lb (3,629 kg)
  • Powerplant:Rolls-Royce Merlin XX V12, 1,390 hp (1,036 kW)

Performance

Armament

[edit] See also

Related development

Comparable aircraft

[edit] References

[edit] Notes

  1. ^ Bridgeman, Leonard. “The Miles M.20.” Jane’s Fighting Aircraft of World War II. London: Studio, 1946. p. 133. ISBN 1 85170 493 0.
  2. ^ "Miles M.20". British Aircraft of World War II. (2003). "Miles M.20". Retrieved: 11 August 2005.
  3. ^ Military.cz (2005). "Miles M.20". Retrieved: 11 August 2005.

[edit] Bibliography

  • Amos, Peter. and Brown, Don Lambert. Miles Aircraft Since 1925, Volume 1. London: Putnam Aeronautical, 2000. ISBN 0-85177-787-0.
  • Brown, Don Lambert. Miles Aircraft Since 1925. London: Putnam & Company Ltd., 1970. ISBN 0-37000-127-3.
  • Green, William. Warplanes of the Second World War, Fighters, Vol. 2. London: Macdonald, 1961.
  • Mondey, David. The Hamlyn Concise Guide to British Aircraft of World War II. London: Chancellor Press, 2002. ISBN 1-85152-668-4.
  • Swanborough, Gordon. British Aircraft at War, 1939-1945. East Sussex, UK: HPC Publishing, 1997. ISBN 0-9531421-0-8.

[edit] External links

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