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A cryogenic platform for space borne instruments with nanokelvin stabilityWe 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.
Document ID
20210002226
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other
External Source(s)
hdl:2014/13032
Authors
Thomassen, J.
Rentz, P.
Gannon, J.
Galloway, S.
Elliott, S.
Craig, J.
Chui, T. C. P.
Bamford, R.
Holmes, W.
Date Acquired
July 16, 2001
Publication Date
July 16, 2001
Publication Information
Publisher: UNKNOWN
Distribution Limits
Public
Copyright
Other
Technical Review
Keywords
space
cryogenics
thermal
control

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