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Three-Dimensional Multifunctional Ablative Thermal Protection SystemA system for fabricating an ablative, 3D fiber-woven thermal protection material, with porosity 0.5-15 percent, reduced thermal conductivity, very low thermal recession, high glass transition temperature, high frontface-backface temperature difference, relatively high mass density, and significant compression strength and tensile strength.
Document ID
20180008164
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Feldman, Jay D.
Wilkinson, Curt G.
Mercer, Kenneth J.
Venkatapathy, Ethiraj
Date Acquired
December 5, 2018
Publication Date
October 23, 2018
Subject Category
Composite Materials
Spacecraft Design, Testing And Performance
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-10,105,909
Patent Application
US-Patent-Appl-SN-15/078,617
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