About: Vickers Type 559   Sponge Permalink

An Entity of Type : dbkwik:resource/AGhloO_nVTaFp7GvOmHv5Q==, within Data Space : 134.155.108.49:8890 associated with source dataset(s)

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. 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.

AttributesValues
rdf:type
rdfs:label
  • Vickers Type 559
rdfs:comment
  • 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. 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.
  • The Vickers (Supermarine) 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. 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.
  • 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.
sameAs
dcterms:subject
dbkwik:military/pr...iPageUsesTemplate
loaded weight main
  • 62190.0
max speed more
  • at altitude
number of props
  • 2(xsd:integer)
combat range
  • 150.0
length alt
  • 20.8 m
span main
  • 42.0
combat range alt
  • 241.0
more performance
  • 1920.0
thrust alt
  • 89 kN
height alt
  • 4.65 m
Type
  • Interceptor
type of prop
  • kerosene/hydrogen peroxide rocket motor
length main
  • 2080.2599999999998
power alt
  • 22 kN
area main
  • 615.0
power main
  • 5000(xsd:integer)
height main
  • 464.82
span alt
  • 12.8 m
missiles
  • 2(xsd:integer)
Manufacturer
  • Vickers-Armstrongs
max speed main
  • 2(xsd:double)
engine (prop)
ceiling main
  • 60000.0
afterburning thrust main
  • 27000(xsd:integer)
empty weight main
  • 41485.0
ceiling more
  • specified by F.155
afterburning thrust alt
  • 120 kN
type of jet
  • turbojet
loaded weight alt
  • 28209.0
area alt
  • 57.1
engine (jet)
jet or prop?
  • both
empty weight alt
  • 18817.0
thrust main
  • 20000(xsd:integer)
number of jets
  • 2(xsd:integer)
plane or copter?
  • plane
ceiling alt
  • 18,000 m
Crew
  • 2(xsd:integer)
Number Built
  • None
ref
  • Supermarine Aircraft since 1914
abstract
  • 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. The Type 559 was an unorthodox canard design with a massive chin air intake, split vertically, for two reheated de Havilland Gyron engines of 4,299 pounds-force (19.12 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 end-plates incorporating twin rudders.
  • 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. 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.
  • The Vickers (Supermarine) 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. 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.
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