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CTE Measurements of Carbon Fibers in ESEMThe strong appeal of carbon fiber reinforced ceramic matrix and carbon-carbon composites arises from their promising high temperature performance within laboratory-simulated nozzle, leading edge and combustor environments. The main drawback in these systems are two fold; namely oxidation affinity and CTE mismatch. To date the emphasis has been on axial CTE mismatch with the push on estimating (component) laminate level data. However, in heterogeneous and anisotropic systems, all failure mechanisms are at micro or nano scales. This paper will report plans and progress on single carbon fibers efforts in order to develop its temperature dependent, anisotropic thermophysical and thermomechanical properties using combination of x-ray spectroscopy and environmental scanning electron microscopy to capture circumferential expansion from 20-900 C in within the SEM chamber. Surface roughness measurements were also determined. Crystallinity was also determined by the quality of the electron diffraction (ED) patterns.
Document ID
20010020055
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Effinger, Michael
(NASA Marshall Space Flight Center Huntsville, AL United States)
Ochoa, Ozden
(Texas A&M Univ. College Station, TX United States)
Munafo, Paul M.
Date Acquired
August 20, 2013
Publication Date
January 1, 2001
Subject Category
Composite Materials
Meeting Information
Meeting: Composites, Materials and Structures
Location: Cocoa Beach, FL
Country: United States
Start Date: January 22, 2001
End Date: January 25, 2001
Funding Number(s)
PROJECT: RTOP 708-72-41
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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