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Design and application of gas-gap heat switchesGas-gap heat switches can serve as an effective means of thermally disconnecting a standby cryocooler when the primary (operating) cooler is connected and vice versa. The final phase of the development and test of a cryogenic heat switch designed for loads ranging from 2 watts at 8 K, to 100 watts at 80 K are described. Achieved heat-switch on/off conductance ratio ranged from 11,000 at 8 K to 2200 at 80 K. A particularly challenging element of heat-switch design is achieving satisfactory operation when large temperatures differentials exist across the switch. A special series of tests and analyses was conducted and used in this Phase-2 activity to evaluate the developed switches for temperature differentials ranging up to 200 K. Problems encountered at the maximum levels are described and analyzed, and means of avoiding the problems in the future are presented. A comprehensive summary of the overall heat-switch design methodology is also presented with special emphasis on lessons learned over the course of the 4-year development effort.
Document ID
19910000909
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Chan, C. K.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Ross, R. G., Jr.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 6, 2013
Publication Date
March 15, 1990
Subject Category
Electronics And Electrical Engineering
Report/Patent Number
JPL-PUBL-90-38
NASA-CR-187339
NAS 1.26:187339
Report Number: JPL-PUBL-90-38
Report Number: NASA-CR-187339
Report Number: NAS 1.26:187339
Accession Number
91N10222
Funding Number(s)
CONTRACT_GRANT: NAS7-918
PROJECT: RTOP 644-11-00-05-81
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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