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Rolls Royce RB145

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Rolls-Royce RB145

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.

Contents

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.

Applications

  • EWR VJ 101
  • Specifications (RB.145)

    Data from Gunston

    General characteristics

  • Type: Single spool turbojet
  • Length:
  • Diameter:
  • Dry weight:
  • Components

  • Compressor: Nine-stage axial
  • Combustors: Annular
  • Performance

  • Maximum thrust: 2,750 lb (12.2 kN)
  • Thrust-to-weight ratio: 6:1
  • References

    Rolls-Royce RB145 Wikipedia