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Vickers Type 559

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Wingspan
  
13 m

Engine type
  
Length
  
21 m

Manufacturer
  
Vickers Type 559 Vickers ArmstrongSupermarine Type 559s Older Brother What If III

The Vickers Type 559 was a supersonic interceptor aircraft design by the British aircraft company Vickers-Armstrongs and was their submission for Operational Requirement F.155 in 1955.

Contents

Vickers Type 559 F155T amp OR329

It was not accepted for further consideration; the most valued submissions being from Armstrong Whitworth and Fairey, however the F.155 requirement was dropped as a result of the 1957 Defence White Paper.

Vickers Type 559 httpsuploadwikimediaorgwikipediacommonsthu

Design and development

The Type 559 was an unorthodox canard design with a massive chin air intake, split vertically, for two reheated de Havilland Gyron engines of 20,000 pounds-force (89 kN) thrust each, placed as in the English Electric Lightning, one above the other. Two de Havilland Spectre Junior rockets were situated each side of the fuselage at wing level. Two Red Hebe or Blue Jay missiles were mounted alongside the upper part of the fuselage between the canard and the mainplane, which had endplates incorporating twin rudders.

Specifications

Data from Supermarine Aircraft since 1914

General characteristics

  • Crew: two (pilot, weapons systems/navigation)
  • Length: 68 ft 3 in (20.8 m)
  • Wingspan: 42 ft (12.8 m)
  • Height: 15 ft 3 in (4.65 m)
  • Wing area: 615 ft² (57.1 m²)
  • Empty weight: 41,485 lb (18,817 kg)
  • Loaded weight: 62,190 lb (28,209 kg)
  • Powerplant:
  • 2 × de Havilland Gyron PS.26/1 turbojet, 20,000 lbf (89 kN) each
  • 2 × De Havilland Spectre Junior kerosene/hydrogen peroxide rocket motor, 5,000 lbf (22 kN) each
  • Performance

  • Maximum speed: 2.5 Mach
  • Service ceiling: 60,000 ft (18,000 m) specified by F.155
  • Endurance: 32 minutes
  • Armament

  • Missiles: 2 × Red Hebe (radar guided) or Blue Jay (heat-seeking) missiles
  • References

    Vickers Type 559 Wikipedia