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Experimental measurement of passive material and structural damping for flexible space structuresAmong the design objectives for large space structures are the maintenance of tight dimensional tolerance and the reduction of settling time after disturbance input. Two options are under consideration for the design of flexible structures to meet these objectives, including an active control option and a passive control option. In connection with both options, it is necessary to include material and structural damping in the design. A description is presented of the results of an experimental investigation of the damping of metallic and fibrous composite materials, taking into account also the analytical modeling and experimental verification of frictional damping schemes. To demonstrate how material and frictional damping can be combined, a simple structural optimization is performed, indicating the potential for significant savings in mass by the addition of frictional dampers.
Document ID
19820061205
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Crawley, E. F.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Sarver, G. L.
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Mohr, D. G.
(MIT Cambridge, MA, United States)
Date Acquired
August 10, 2013
Publication Date
September 1, 1982
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
IAF PAPER 82-380
Report Number: IAF PAPER 82-380
Accession Number
82A44740
Funding Number(s)
CONTRACT_GRANT: NAGW-21
Distribution Limits
Public
Copyright
Other

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