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Space flight cable model development

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dc.contributor.author Spak, Kaitlin
dc.date.accessioned 2013-12-18T17:50:28Z
dc.date.available 2013-12-18T17:50:28Z
dc.date.issued 2013-04-18
dc.identifier.citation Virginia Space Grant Consortium Student Research Conference, Norfolk, Virginia, April 18, 2013. en_US
dc.identifier.clearanceno 13-2097
dc.identifier.uri http://hdl.handle.net/2014/44131
dc.description.abstract This work concentrates the modeling efforts presented in last year’s VSGC conference paper, “Model Development for Cable-Harnessed Beams.” The focus is narrowed to modeling of space-flight cables only, as a reliable damped cable model is not yet readily available and is necessary to continue modeling cable-harnessed space structures. New experimental data is presented, eliminating the low-frequency noise that plagued the first year’s efforts. The distributed transfer function method is applied to a single section of space flight cable for Euler-Bernoulli and shear beams. The work presented here will be developed into a damped cable model that can be incorporated into an interconnected beam-cable system. The overall goal of this work is to accurately predict natural frequencies and modal damping ratios for cabled space structures. en_US
dc.description.sponsorship NASA/JPL en_US
dc.language.iso en_US en_US
dc.publisher Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2013 en_US
dc.subject space structures en_US
dc.subject space flight cables en_US
dc.subject reliability en_US
dc.subject testing en_US
dc.title Space flight cable model development en_US
dc.type Other en_US


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