About: Rolls-Royce RB.145     Goto   Sponge   NotDistinct   Permalink

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The Rolls-Royce RB.145 was a British jet engine designed in the early-1960s by Rolls-Royce for use as a lightweight VTOL lift and cruise engine. Developed from the Rolls-Royce RB108 the RB.145 featured more accessories and a higher thrust rating. Six engines developed by MAN Turbo were fitted to the first prototype of the EWR VJ 101 experimental German fighter aircraft, achieving supersonic flight by July 1964. Reheated versions of the RB.145 with a thrust of 3,650 lb (16.2 kN) were fitted to the second EWR VJ 101 with the intention of reaching Mach 1.4.

AttributesValues
rdfs:label
  • Rolls-Royce RB.145 (fr)
  • Rolls-Royce RB.145 (en)
rdfs:comment
  • The Rolls-Royce RB.145 was a British jet engine designed in the early-1960s by Rolls-Royce for use as a lightweight VTOL lift and cruise engine. Developed from the Rolls-Royce RB108 the RB.145 featured more accessories and a higher thrust rating. Six engines developed by MAN Turbo were fitted to the first prototype of the EWR VJ 101 experimental German fighter aircraft, achieving supersonic flight by July 1964. Reheated versions of the RB.145 with a thrust of 3,650 lb (16.2 kN) were fitted to the second EWR VJ 101 with the intention of reaching Mach 1.4. (en)
  • Le Rolls-Royce RB.145 était un turboréacteur conçu au début des années 1960 par la société britannique Rolls-Royce Limited, pour être utilisé comme moteur léger de sustentation et de croisière pour avions à décollages verticaux. (fr)
foaf:depiction
  • http://commons.wikimedia.org/wiki/Special:FilePath/EWR_VJ101.jpg
  • http://commons.wikimedia.org/wiki/Special:FilePath/Rolls-Royce_RB.145_RRHT_Derby.jpg
dcterms:subject
Wikipage page ID
Wikipage revision ID
Link from a Wikipage to another Wikipage
Link from a Wikipage to an external page
  • http://www.eads.com/xml/content/OF00000000400004/5/81/543815.jpg
sameAs
specfuelcon
  • ::Wet: ::Dry: *Oil consumption: (en)
thrust
  • ::Take-off, wet: ::Take-off, dry: (en)
thrust/weight
turbine
dbp:wikiPageUsesTemplate
thumbnail
national origin
  • United Kingdom (en)
manufacturer
ref
  • Aircraft engines of the World 1964/65. (en)
related
  • *Rolls-Royce RB108 (en)
type
has abstract
  • The Rolls-Royce RB.145 was a British jet engine designed in the early-1960s by Rolls-Royce for use as a lightweight VTOL lift and cruise engine. Developed from the Rolls-Royce RB108 the RB.145 featured more accessories and a higher thrust rating. Six engines developed by MAN Turbo were fitted to the first prototype of the EWR VJ 101 experimental German fighter aircraft, achieving supersonic flight by July 1964. Reheated versions of the RB.145 with a thrust of 3,650 lb (16.2 kN) were fitted to the second EWR VJ 101 with the intention of reaching Mach 1.4. (en)
  • Le Rolls-Royce RB.145 était un turboréacteur conçu au début des années 1960 par la société britannique Rolls-Royce Limited, pour être utilisé comme moteur léger de sustentation et de croisière pour avions à décollages verticaux. (fr)
combustion
  • Annular with duplex burners (en)
compressor
  • Nine-stage axial-flow (en)
developed from
first run
  • April 1961 (en)
fueltype
  • JP-1 or JP-4 (en)
lists
  • *List of aircraft engines (en)
major applications
oilsystem
  • Return system at (en)
see also
  • *Rolls-Royce RB162 (en)
prov:wasDerivedFrom
page length (characters) of wiki page
foaf:isPrimaryTopicOf
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is Wikipage redirect of
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