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Advanced General Aviation Turbine Engine (GATE) studyThe small engine technology requirements suitable for general aviation service in the 1987 to 1988 time frame were defined. The market analysis showed potential United States engines sales of 31,500 per year providing that the turbine engine sales price approaches current reciprocating engine prices. An optimum engine design was prepared for four categories of fixed wing aircraft and for rotary wing applications. A common core approach was derived from the optimum engines that maximizes engine commonality over the power spectrum with a projected price competitive with reciprocating piston engines. The advanced technology features reduced engine cost, approximately 50 percent compared with current technology.
Document ID
19790021018
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Smith, R.
(Teledyne CAE Toledo, OH, United States)
Benstein, E. H.
(Teledyne CAE Toledo, OH, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1979
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
TELEDYNE-CAE-1600
NASA-CR-159624
Report Number: TELEDYNE-CAE-1600
Report Number: NASA-CR-159624
Accession Number
79N29189
Funding Number(s)
CONTRACT_GRANT: NAS3-20757
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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