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Study of buoyancy systems for flight vehiclesThe performance potential of buoyant systems and flexible structures used in air vehicles for short-haul passenger transportation is discussed. The study was intended only to determine if sufficient performance potential existed, and to provide a focus for a more extensive design study, if such a study appeared desirable. A relatively conventional helium system was examined along with a more unusual configuration employing hot-air as the buoyant fluid. Both configurations were examined in the VTOL and STOL modes of operation. The helium system appears to have some superiority in the VTOL mode, while the hot-air system has a superiority in the STOL mode. Both configurations exhibit sufficient performance potential to suggest that a much more extensive design study might well be undertaken.
Document ID
19730008287
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Havill, C. D.
(NASA Ames Research Center Moffett Field, CA, United States)
Williams, L. J.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1972
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-62168
Report Number: NASA-TM-X-62168
Accession Number
73N17014
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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