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A turboshaft engine differs from a turboprop in that its shaft power drives

  • A.A second compressor stage
  • B.A rotor, generator or pump
  • C.A propeller through a gearbox
  • D.Nothing at all

Answer: B

The gas generator is essentially identical and only the load differs, which is why the same core often appears in both roles. Having no propeller means there is no residual jet thrust worth counting in the output rating.

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