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Active CryoCubeSatThe Active CryoCubeSat project will demonstrate an advanced thermal control system for a 6-Unit (6U) CubeSat platform. A miniature, active thermal control system, in which a fluid is circulated in a closed loop from thermal loads to radiators, will be developed. A miniature cryogenic cooler will be integrated with this system to form a two-stage thermal control system. Key components will be miniaturized by using advanced additive manufacturing techniques resulting in a thermal testbed for proving out these technologies. Previous CubeSat missions have not tackled the problem of active thermal control systems nor have any past or current CubeSat missions included cryogenic instrumentation. This Active CryoCubeSat development effort will provide completely new capacities for CubeSats and constitutes a major advancement over the state-of-the-art in CubeSat thermal control.
Document ID
20160007914
Acquisition Source
Ames Research Center
Document Type
Other - Brief Communication/Note
Authors
Swenson, Charles
(Utah State Univ. Logan, UT, United States)
Date Acquired
June 27, 2016
Publication Date
April 20, 2016
Subject Category
Fluid Mechanics And Thermodynamics
Spacecraft Design, Testing And Performance
Report/Patent Number
FS-2016-04-02-ARC
ARC-E-DAA-TN31590
Funding Number(s)
CONTRACT_GRANT: NNX15AW56A
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
CubeSat
Cryocooler
Active thermal control
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