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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.

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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. (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)
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  • 25627971 (xsd:integer)
dbo:wikiPageLength
  • 4398 (xsd:nonNegativeInteger)
dbo:wikiPageRevisionID
  • 1065833061 (xsd:integer)
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dbp:combustion
  • Annular with duplex burners (en)
dbp:compressor
  • Nine-stage axial-flow (en)
dbp:developedFrom
dbp:firstRun
  • April 1961 (en)
dbp:fueltype
  • JP-1 or JP-4 (en)
dbp:lists
  • *List of aircraft engines (en)
dbp:majorApplications
dbp:manufacturer
dbp:nationalOrigin
  • United Kingdom (en)
dbp:oilsystem
  • Return system at (en)
dbp:ref
  • Aircraft engines of the World 1964/65. (en)
dbp:related
  • *Rolls-Royce RB108 (en)
dbp:seeAlso
  • *Rolls-Royce RB162 (en)
dbp:specfuelcon
  • ::Wet: ::Dry: *Oil consumption: (en)
dbp:thrust
  • ::Take-off, wet: ::Take-off, dry: (en)
dbp:thrust/weight
  • 6.080000 (xsd:double)
dbp:turbine
  • 2 (xsd:integer)
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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. (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)
rdfs:label
  • Rolls-Royce RB.145 (fr)
  • Rolls-Royce RB.145 (en)
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