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Advanced composites: Environmental effects on selected resin matrix materialsThe effects that expected space flight environment has upon the mechanical properties of epoxy and polyimide matrix composites were analyzed. Environmental phenomena covered water immersion, high temperature aging, humidity, lightning strike, galvanic action, electromagnetic interference, thermal shock, rain and sand erosion, and thermal/vacuum outgassing. The technology state-of-the-art for graphite and boron reinforced epoxy and polyimide matrix materials is summarized to determine the relative merit of using composites in the space shuttle program. Resin matrix composites generally are affected to some degree by natural environmental phenomena with polyimide resin matrix materials less affected than epoxies.
Document ID
19760024211
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Welhart, E. K.
(McDonnell-Douglas Technical Services Co., Inc. Houston, TX, United States)
Date Acquired
September 3, 2013
Publication Date
March 31, 1976
Subject Category
Composite Materials
Report/Patent Number
NASA-CR-150938
DN-1.2-DN-B0104-2
Report Number: NASA-CR-150938
Report Number: DN-1.2-DN-B0104-2
Accession Number
76N31299
Funding Number(s)
CONTRACT_GRANT: NAS9-14960
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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