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A helium-3 refrigerator employing capillary confinement of liquid cryogenA condensation refrigerator suitable for operation in a zero gravity space environment was constructed. The condensed liquid refrigerant is confined by surface tension inside a porous metal matrix. Helium-4 and helium-3 gases were condensed and held in a copper matrix. Evaporative cooling of confined liquid helium-4 resulted in a temperature of 1.4K. Using a zeolite adsorption pump external to the cryostat, a temperature of 0.6 K was achieved through evaporative cooling of liquid helium-3. The amount of time required for complete evaporation of a controlled mass of liquid helium-4 contained in the copper matrix was measured as a function of the applied background power. For heating powers below 18 mW the measured times are consistent with the normal boiling of the confined volume of liquid refrigerant. At background powers above 18 mW the rapid rise in the temperature of the copper matrix the signature of the absence of confined liquid occurs in a time a factor of two shorter than that expected on the basis of an extrapolation of the low power data.
Document ID
19840007285
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ennis, D. J.
(NASA Ames Research Center Moffett Field, CA, United States)
Kittel, P.
(NASA Ames Research Center Moffett Field, CA, United States)
Brooks, W.
(NASA Ames Research Center Moffett Field, CA, United States)
Miller, A.
(NASA Ames Research Center Moffett Field, CA, United States)
Spivak, A. L.
(Transbay Electronics Richmond, Calif., United States)
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
84N15353
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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