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Lift/cruise fan V/STOL technology aircraft design definition study. Volume 2: Propulsion transmission system designTwo types of lift/cruise fan technology aircraft were conceptually designed. One aircraft used turbotip fans pneumatically interconnected to three gas generators, and the other aircraft used variable pitch fans mechanically interconnected to three turboshaft engines. The components of each propulsion transmission system were analyzed and designed to the depth necessary to determine areas of risk, development methods, performance, weights and costs. The types of materials and manufacturing processes were identified to show that the designs followed a low cost approach. The lift/cruise fan thrust vectoring hoods, which are applicable to either aircraft configuration, were also evaluated to assure a low cost/low risk approach.
Document ID
19770009071
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Obrien, W. J.
(McDonnell Aircraft Co. Saint Louis, MO, United States)
Date Acquired
September 3, 2013
Publication Date
November 18, 1976
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
MDC-A4551-VOL-2
NASA-CR-151932
Report Number: MDC-A4551-VOL-2
Report Number: NASA-CR-151932
Accession Number
77N16014
Funding Number(s)
CONTRACT_GRANT: NAS2-9245
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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