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Permeability After Impact Testing of Composite LaminatesSince composite laminates are beginning to be identified for use in reusable launch vehicle propulsion systems, an understanding of their permeance is needed. A foreign object impact event can cause a localized area of permeability (leakage) in a polymer matrix composite and it is the aim of this study to assess a method of quantifying permeability-after-impact results. A simple test apparatus is presented and variables that could affect the measured values of permeability-after-impact were assessed. Once it was determined that valid numbers were being measured, a fiber/resin system was impacted at various impact levels and the resulting permeability measured, first with a leak check solution (qualitative) then using the new apparatus (quantitative). The results showed that as the impact level increased, so did the measured leakage. As the pressure to the specimen was increased, the leak rate was seen to increase in a non-linear fashion for almost all of the specimens tested.
Document ID
20030064094
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Nettles, Alan T.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2003
Subject Category
Composite Materials
Meeting Information
Meeting: SAMPE 2003 Symposium and Exhibition
Location: Long Beach, CA
Country: United States
Start Date: May 11, 2003
End Date: May 15, 2003
Sponsors: Society for the Advancement of Materials and Process Engineering
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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