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A cryogenic platform for space borne instruments with nanokelvin stability

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dc.contributor.author Holmes, W. en_US
dc.contributor.author Bamford, R. en_US
dc.contributor.author Chui, T. C. P. en_US
dc.contributor.author Craig, J. en_US
dc.contributor.author Elliott, S. en_US
dc.contributor.author Galloway, S. en_US
dc.contributor.author Gannon, J. en_US
dc.contributor.author Rentz, P. en_US
dc.contributor.author Thomassen, J. en_US
dc.date.accessioned 2004-09-22T23:53:13Z
dc.date.available 2004-09-22T23:53:13Z
dc.date.issued 2001-07-16 en_US
dc.identifier.citation Cryogenic Engineering Conference en_US
dc.identifier.citation Madison, WI, USA en_US
dc.identifier.clearanceno 01-1508 en_US
dc.identifier.uri http://hdl.handle.net/2014/13032
dc.description.abstract We describe the design and test of a modular probe structure to allow nK control of <8 kg space borne instruments operated at liquid helium temperatures for the Low Temperature Microgravity Physics Program. en_US
dc.format.extent 1365657 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other space cryogenics thermal control en_US
dc.title A cryogenic platform for space borne instruments with nanokelvin stability en_US


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