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Uniaxial and biaxial tensioning effects on thin membrane materialsThin laminated membranes are being considered for various surface applications on future large space structural systems. Some of the thin membranes would be stretched across or between structural members with the requirement that the membrane be maintained within specified limits of smoothness which would be dictated by the particular applications such as antenna reflector requirements. The multiaxial tensile force required to maintain the smoothness in the membrane needs to be determined for use in the structure design. Therefore, several types of thicknesses of thin membrane materials have been subjected to varied levels of uniaxial and biaxial tensile loads. During the biaxial tests, deviations of the material surface smoothness were measured by a noncontacting capacitance probe. Basic materials consisted of composites of vacuum deposited aluminum on Mylar and Kapton ranging in thickness from 0.00025 in (0.000635 cm) to 0.002 in (0.00508 cm). Some of the material was reinforced with Kevlar and Nomex scrim. The uniaxial tests determined the material elongation and tensile forces up to ultimate conditions. Biaxial tests indicated that a relatively smooth material surface could be achieved with tensile force of approximately 1 to 15 Newtons per centimeter, depending upon the material thickness and/or reinforcement.
Document ID
19800017896
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Hinson, W. F.
(NASA Langley Research Center Hampton, VA, United States)
Goslee, J. W.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
June 1, 1980
Subject Category
Composite Materials
Report/Patent Number
NASA-TM-81812
Accession Number
80N26395
Funding Number(s)
PROJECT: RTOP 542-01-13-15
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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