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Regeneration efficiency, shuttle heat loss and thermal conductivity in epoxy-composite annualr gap regenerators from 4K to 80KA test apparatus designed to simulate a section of a Stirling cycle cryocooler was built. Measurements of regeneration efficiency, shuttle heat loss and thermal conductivity reported for several regenerator test sections. The test composites were epoxy glass, epoxy glass with lead particles, epoxy glass with activated charcoal and epoxy graphite. Losses measured for these materials were approximately the same. Losses are in good agreement with those calculated theoretically for an epoxy glass (C-10) composite. The implications of these results on cryocooler design are discussed.
Document ID
19840007267
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Myrtle, K.
(Simon Fraser Univ. Burnaby British Columbia, Canada)
Cygax, S.
(Simon Fraser Univ. Burnaby British Columbia, Canada)
Plateel, C.
(Simon Fraser Univ. Burnaby British Columbia, Canada)
Winter, C.
(Simon Fraser Univ. Burnaby British Columbia, Canada)
Date Acquired
August 12, 2013
Publication Date
December 1, 1983
Publication Information
Publication: NASA. Goddard Space Flight Center Refrig. for for Cryogenic Sensors
Subject Category
Engineering (General)
Accession Number
84N15335
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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