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A guide to structural factors for advanced composites used on spacecraftThe use of composite materials in spacecraft systems is constantly increasing. Although the areas of composite design and fabrication are maturing, they remain distinct from the same activities performed using conventional materials and processes. This has led to some confusion regarding the precise meaning of the term 'factor of safety' as it applies to these structures. In addition, composite engineering introduces terms such as 'knock-down factors' to further modify material properties for design purposes. This guide is intended to clarify these terms as well as their use in the design of composite structures for spacecraft. It is particularly intended to be used by the engineering community not involved in the day-to-day composites design process. An attempt is also made to explain the wide range of factors of safety encountered in composite designs as well as their relationship to the 1.4 factor of safety conventionally applied to metallic structures.
Document ID
19920011566
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Vanwagenen, Robert
(Vitro Corp. Washington, DC, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1989
Subject Category
Composite Materials
Report/Patent Number
NASA-CR-186010
NAS 1.26:186010
Report Number: NASA-CR-186010
Report Number: NAS 1.26:186010
Accession Number
92N20808
Funding Number(s)
CONTRACT_GRANT: NASW-4311
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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