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The Bristol Siddeley BS.100 is a British twin-spool, vectored thrust, turbofan aero engine that first ran in 1960. The engine was designed and built in limited numbers by Bristol Siddeley Engines Limited. The project was cancelled in early 1965.

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rdfs:label
  • Bristol Siddeley BS.100 (en)
  • Bristol Siddeley BS.100 (fr)
  • ブリストル・シドレー BS.100 (ja)
rdfs:comment
  • The Bristol Siddeley BS.100 is a British twin-spool, vectored thrust, turbofan aero engine that first ran in 1960. The engine was designed and built in limited numbers by Bristol Siddeley Engines Limited. The project was cancelled in early 1965. (en)
  • Le Bristol Siddeley BS.100 était un turbofan britannique, à double corps et à poussée vectorielle, qui fut mis en route pour la première fois en 1960. Le moteur fut conçu et produit en nombre limité par Bristol Siddeley Engines, Ltd., puis le projet fut annulé début 1965. (fr)
  • ブリストル・シドレー BS.100はイギリスの2軸式推力偏向型ターボファンエンジンである。1960年に初めて運転され少数がブリストル・シドレー社によって設計、生産された。計画は1965年初頭に中止された。 (ja)
foaf:depiction
  • http://commons.wikimedia.org/wiki/Special:FilePath/Bristol_Siddeley_BS100.jpg
dcterms:subject
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Wikipage revision ID
Link from a Wikipage to another Wikipage
Link from a Wikipage to an external page
sameAs
similar engines
  • *Rolls-Royce/MAN Turbo RB193 (en)
specfuelcon
thrust
turbine
  • HP cooled single-stage with 2-stage uncooled LP turbines (en)
turbinetemp
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thumbnail
diameter
  • fan (en)
length
  • fan entry to exhaust cone truncation (en)
manufacturer
ref
  • Pegasus:The Heart Of The Harrier. (en)
related
  • *Rolls-Royce Pegasus (en)
type
has abstract
  • The Bristol Siddeley BS.100 is a British twin-spool, vectored thrust, turbofan aero engine that first ran in 1960. The engine was designed and built in limited numbers by Bristol Siddeley Engines Limited. The project was cancelled in early 1965. (en)
  • Le Bristol Siddeley BS.100 était un turbofan britannique, à double corps et à poussée vectorielle, qui fut mis en route pour la première fois en 1960. Le moteur fut conçu et produit en nombre limité par Bristol Siddeley Engines, Ltd., puis le projet fut annulé début 1965. (fr)
  • ブリストル・シドレー BS.100はイギリスの2軸式推力偏向型ターボファンエンジンである。1960年に初めて運転され少数がブリストル・シドレー社によって設計、生産された。計画は1965年初頭に中止された。 (ja)
bypass
compression
compressor
  • Two-spool axial flow, 4-stage LP compressor fan, with 7-stage HP compressor (en)
first run
fueltype
  • Kerosene (en)
lists
  • * List of aircraft engines (en)
major applications
number built
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page length (characters) of wiki page
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is Link from a Wikipage to another Wikipage of
is Wikipage redirect of
is eng1 name of
is foaf:primaryTopic of
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