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Microstructural evolution of NARloy-Z at elevated temperaturesMicrostructural evolution was studied in samples of wrought and vacuum plasma sprayed (VPS) NARloy-Z exposed to temperatures up to 970 C (1,780 F) for up to 60 h. Samples were heated in a vacuum furnace, followed by rapid quenching in helium (He) gas at a cooling rate of 166 C (300 F) per second. Microstructural analyses were conducted using optical microscopy, scanning electron microscopy (SEM), and electron probe microanalysis (EPMA). In both the wrought and VPS conditions, precipitates rich in silver (Ag) and zirconium (Zr) were present in the matrix and at the grain boundaries even after long exposure to elevated temperatures. Islands rich in oxygen (O2) and Zr were also observed, as well as incipient melting at the grain boundary triple points. Results indicated that the alloy cannot be homogenized by heat treatment at elevated temperatures.
Document ID
19940009242
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Singh, J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Jerman, G.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Bhat, B. N.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Poorman, R.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1993
Subject Category
Metallic Materials
Report/Patent Number
NAS 1.15:108419
NASA-TM-108419
Report Number: NAS 1.15:108419
Report Number: NASA-TM-108419
Accession Number
94N13715
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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