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The effect of temperature cycling typical of low earth orbit satellites on thin films of YBa2Cu3O(7-x)Thin films of YBa2Cu3O(7-x) (YBCO) were temperature cycled to simulate conditions of a low earth orbit satellite. In one series of tests, epitaxial and polycrystalline YBCO films were cycled between temperatures of +/- 80 C in vacuum and in nitrogen for hundreds of cycles. The room temperature resistance of an epitaxial YBCO film increased by about 10 percent, but the superconducting transition temperature was unchanged. The largest changes were for a polycrystalline YBCO film on oxidized silicon with a zirconia buffer layer, for which the transition temperature decreased by 3 K. An extended test was carried out for epitaxial films. After 3200 cycles (corresponding to about 230 days in space), transition temperatures and critical current densities remained unchanged.
Document ID
19920012429
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mogro-Campero, A.
(General Electric Co. Schenectady, NY., United States)
Turner, L. G.
(General Electric Co. Schenectady, NY., United States)
Bogorad, A.
(General Electric Co. Princeton, NJ., United States)
Herschitz, R.
(General Electric Co. Princeton, NJ., United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1991
Publication Information
Publication: NASA. Goddard Space Flight Center, AMSAHTS 1990: Advances in Materials Science and Applications of High Temperature Superconductors
Subject Category
Solid-State Physics
Accession Number
92N21672
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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