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Permeability testing of impacted composite laminates for use on reusable launch vehicles / A.T. Nettles.

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Format:
Book
Government document
Author/Creator:
Nettles, A. T. (Alan T.), author.
Contributor:
George C. Marshall Space Flight Center, issuing body.
Series:
NASA technical memorandum ; 2001-210799.
NASA/TM ; 2001-210799
Language:
English
Genre:
Online resources.
Physical Description:
1 online resource (v, 21 pages) : illustrations.
Place of Publication:
MSFC, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, February 2001.
Summary:
Since 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 nonlinear fashion for almost all the specimens tested
Notes:
"February 2001."
"Performing organization: George C. Marshall Space Flight Center"--Report documentation page.
Includes bibliographical references (page 21).
Description based on online resource; title from PDF title page (NASA, viewed Nov. 29, 2017).
Other Format:
Microfiche version: Permeability Testing of Impacted Composite Laminates for Use on Reusable Launch Vehicles
Microfiche version: Nettles, A. T. (Alan T.). Permeability testing of impacted composite laminates for use on reusable launch vehicles
OCLC:
703644813

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