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Vibrations and structureborne noise in space stationTheoretical models were developed capable of predicting structural response and noise transmission to random point mechanical loads. Fiber reinforced composite and aluminum materials were considered. Cylindrical shells and circular plates were taken as typical representatives of structural components for space station habitability modules. Analytical formulations include double wall and single wall constructions. Pressurized and unpressurized models were considered. Parametric studies were conducted to determine the effect on structural response and noise transmission due to fiber orientation, point load location, damping in the core and the main load carrying structure, pressurization, interior acoustic absorption, etc. These analytical models could serve as preliminary tools for assessing noise related problems, for space station applications.
Document ID
19860011014
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Vaicaitis, R.
(Columbia Univ. New York, NY, United States)
Date Acquired
September 5, 2013
Publication Date
December 31, 1985
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CR-176520
NAS 1.26:176520
Report Number: NASA-CR-176520
Report Number: NAS 1.26:176520
Accession Number
86N20485
Funding Number(s)
CONTRACT_GRANT: NAG1-541
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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