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Solid Freeform Fabrication of Continuous Fiber Reinforced Composites for Propulsion ApplicationsMonolithic ceramics lack the fracture toughness necessary to be considered for propulsion related applications. To be used for such applications, materials must possess low density, high elastic modulus, a low thermal expansion coefficient, high thermal conductivity, excellent erosion and oxidation/corrosion resistance, and flaw-insensitivity. They will in many cases also be required to possess the ability to be joined, to survive thermal cycling and multi-axial stress states, and for reusable applications the materials must maintain the above attributes after prolonged exposure to extremely harsh chemical environments. The final and possibly most important attributes for these materials are the need to be of low cost and readily available in large quantities.
Document ID
20010067260
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Vaidyanathan, R.
(Advanced Ceramics Research, Inc. Tucson, AZ United States)
Fox, M.
(Advanced Ceramics Research, Inc. Tucson, AZ United States)
Walish, J.
(Advanced Ceramics Research, Inc. Tucson, AZ United States)
Rigali, M.
(Advanced Ceramics Research, Inc. Tucson, AZ United States)
Cipriani, R.
(Advanced Ceramics Research, Inc. Tucson, AZ United States)
Gillespie, J.
(Delaware Univ. Newark, DE United States)
Yarlagadda, S.
(Delaware Univ. Newark, DE United States)
Effinger, M.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
August 20, 2013
Publication Date
February 1, 2001
Publication Information
Publication: Proceedings of The 4th Conference on Aerospace Materials, Processes, and Environmental Technology
Subject Category
Composite Materials
Funding Number(s)
CONTRACT_GRANT: NAS8-00084
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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