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Additional design studies of the NASA/Navy lift/cruise fanAdditional preliminary design studies were performed for a turbotip lift/cruise fan propulsion system for a Navy multimission aircraft. The LCF459/J97 propulsion system was previously designed for this application. These studies extended the analysis in areas of (1) scroll commonality, (2) increased engine-out contingency ratings, (3) mounting systems, (4) manufacturing cost reductions, and (5) vulnerability.
Document ID
19760010056
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 3, 2013
Publication Date
January 5, 1976
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-134928
R76AEG152
Report Number: NASA-CR-134928
Report Number: R76AEG152
Accession Number
76N17144
Funding Number(s)
CONTRACT_GRANT: NAS3-19411
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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