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Processing eutectics in spaceThe examination of the Ni-Mo-Al system is discussed. Experiments were performed to examine the role of thermal gradient magnitude at the solidifying interface on the geometrical regularity of the microstructure. The difficulty in measuring the thermal gradient in the melt using superheat temperatures as high as 1800 C resulted in the examination of three liquid temperature gradient ranges. Examination of the microstructure from directionally solidified ingots using transverse sections indicated that the highest gradient runs produced microstructure of no greater regularity than runs made at lower gradients. For the Ni-Al-Mo monovariant eutectic system, the magnitude of the thermal gradient at the solidifying interface is not a controlling parameter with respect to the geometrical regularity of the microstructure, provided it is sufficient to satisfy the gradient/rate ratio needed to produce a planar interface growth.
Document ID
19770016190
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Douglas, F. C.
(United Technologies Research Center East Hartford, CT, United States)
Galasso, S. F.
(United Technologies Research Center East Hartford, CT, United States)
Date Acquired
September 3, 2013
Publication Date
February 10, 1977
Subject Category
Astronautics (General)
Report/Patent Number
NASA-CR-150251
R77-911721-11
Report Number: NASA-CR-150251
Report Number: R77-911721-11
Accession Number
77N23134
Funding Number(s)
CONTRACT_GRANT: NAS8-29669
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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