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The high temperature creep behavior of oxides and oxide fibersA thorough review of the literature was conducted on the high-temperature creep behavior of single and polycrystalline oxides which potentially could serve as fiber reinforcements in ceramics or metal matrix applications. Sapphire when oriented with the basal plane perpendicular to the fiber axis (c-axis oriented) is highly creep resistant at temperatures in excess of 1600 C and applied loads of 100 MPa and higher. Pyramidal slip is preferentially activated in sapphire under these conditions and steady-state creep rates in the range of 10(exp -7) to 10 (exp -8)/s were reported. Data on the creep resistance of polycrystalline beryllia suggest that C-axiz oriented single crystal beryllia may be a viable candidate as a fiber reinforcement material; however, the issure of fabricability and moisture sensitivity must be addressed for this material. Yttrium aluminum garnet (YAG) also appears to be a fiber candidate material having a high resistance to creep which is due to it's complex crystal structure and high Peierl resistance. The high creep resistance of garnet suggests that there may be other complex ternary oxides such as single crystal mullite which may also be candidate materials for fiber reinforcements. Finally, CVD and single crystal SiC, although not oxides, do possess a high resistance to creep in the temperature range between 1550 and 1850 C and under stresses of 110 to 220 MPa. From a review of the literature, it appears that for high creep resistant applications sapphire, silicon carbide, yttrium aluminum garnet, mullite, and beryllia are desirable candidate materials which require further investigation.
Document ID
19910010928
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Jones, Linda E.
(Pennsylvania State Univ. University Park, PA, United States)
Tressler, Richard E.
(Pennsylvania State Univ. University Park, PA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1991
Subject Category
Composite Materials
Report/Patent Number
NASA-CR-187060
CAM-9009
NAS 1.26:187060
Report Number: NASA-CR-187060
Report Number: CAM-9009
Report Number: NAS 1.26:187060
Accession Number
91N20241
Funding Number(s)
PROJECT: RTOP 510-01-50
CONTRACT_GRANT: NAGW-1381
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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