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Recent Advances in the Development of Thick-Section Melt-Infiltrated C/SiC CompositesUsing a pressureless melt infiltration and in situ reaction process to form the silicon carbide (SiC) matrix, Ultramet has been developing a means to rapidly fabricate ceramic matrix composites (CMCs) targeting thicker sections. The process also employs a unique route for the application of oxide fiber interface coatings designed to protect the fiber and impart fiber-matrix debond. Working toward a 12 inch diameter, 2.5 inch thick demonstrator component, the effect of various processing parameters on room temperature flexure strength is being studied with plans for more extensive elevated temperature mechanical strength evaluation to follow this initial optimization process.
Document ID
20040028006
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Babcock, Jason R.
(Ultramet Co. Pacoima, CA, United States)
Ramachandran, Gautham
(Ultramet Co. Pacoima, CA, United States)
Williams, Brian E.
(Ultramet Co. Pacoima, CA, United States)
Effinger, Michael R.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 21, 2013
Publication Date
January 1, 2004
Subject Category
Composite Materials
Meeting Information
Meeting: 28th Annual Conference on Composites, Materials and Structures
Location: Cocoa Beach, FL
Country: United States
Start Date: January 26, 2004
End Date: January 30, 2004
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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