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Characterization and modeling of an advanced flexible thermal protection material for space applicationsThis paper describes experimental and analytical characterization of a new flexible thermal protection material known as Tailorable Advanced Blanket Insulation (TABI). This material utilizes a three-dimensional ceramic fabric core structure and an insulation filler. TABI is the leading candidate for use in deployable aeroassisted vehicle designs. Such designs require extensive structural modeling, and the most significant in-plane material properties necessary for model development are measured and analytically verified in this study. Unique test methods are developed for damping measurements. Mathematical models are developed for verification of the experimental modulus and damping data, and finally, transverse properties are described in terms of the inplane properties through use of a 12-dof finite difference model of a simple TABI configuration.
Document ID
19910047222
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Clayton, Joseph P.
(Remtech, Inc. Huntsville, AL, United States)
Tinker, Michael L.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1991
Subject Category
Composite Materials
Report/Patent Number
AIAA PAPER 91-1047
Meeting Information
Meeting: AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
Location: Baltimore, MD
Country: United States
Start Date: April 8, 1991
End Date: April 10, 1991
Accession Number
91A31845
Distribution Limits
Public
Copyright
Other

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