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Design definition study of a lift/cruise fan technology V/STOL airplane: SummaryA two-engine three-fan V/STOL airplane was designed to fulfill naval operational requirements. A multimission airplane was developed from study of specific point designs. Based on the multimission concept, airplanes were designed to demonstrate and develop the technology and operational procedures for this class of aircraft. Use of interconnected variable pitch fans led to a good balance between high thrust with responsive control and efficient thrust at cruise speeds. The airplanes and their characteristics are presented.
Document ID
19760011013
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Zabinsky, J. M.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Higgins, H. C.
(Boeing Commercial Airplane Co. Seattle, WA, United States)
Date Acquired
September 3, 2013
Publication Date
August 15, 1975
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
D6-42647
NASA-CR-137749
Report Number: D6-42647
Report Number: NASA-CR-137749
Accession Number
76N18101
Funding Number(s)
CONTRACT_GRANT: NAS2-6563
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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