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A CMC database for use in the next generation launch vehicles (rockets)Ceramic matrix composites (CMC's) are being envisioned as the state-of-the-art material capable of handling the tough structural and thermal demands of advanced high temperature structures for programs such as the SSTO (Single Stage to Orbit), HSCT (High Speed Civil Transport), etc. as well as for evolution of the industrial heating systems. Particulate, whisker and continuous fiber ceramic matrix (CFCC) composites have been designed to provide fracture toughness to the advanced ceramic materials which have a high degree of wear resistance, hardness, stiffness, and heat and corrosion resistance but are notorious for their brittleness and sensitivity to microscopic flaws such as cracks, voids and impurity.
Document ID
19950012578
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mahanta, Kamala
(State Univ. of New York Oneonta, NY, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1994
Publication Information
Publication: Alabama Univ., Research Reports: 1994 NASA(ASEE Summer Faculty Fellowship Program
Subject Category
Launch Vehicles And Space Vehicles
Accession Number
95N18993
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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