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Active Thermal Architecture for Cryogenic Optical Instrumentation (ATACOI)The Active Thermal Architecture for Cryogenic Optical Instrumentation (ATACOI) project will demonstrate an advanced thermal control system for CubeSats and enable the use of cryogenic electro-optical instrumentation on small satellite platforms. Specifically, the project focuses on the development of a deployable solar tracking radiator, a rotationally flexible rotary union fluid joint, and a thermal/vibrational isolation system for miniature cryogenic detectors. This technology will represent a significant improvement over the current state of the art for CubeSat thermal control, which generally relies on simple passive and conductive methods.
Document ID
20180002969
Acquisition Source
Ames Research Center
Document Type
Other - Brief Communication/Note
Authors
Swenson, Charles
(Utah State Univ. Logan, UT, United States)
Hunter, Roger C.
(NASA Ames Research Center Moffett Field, CA, United States)
Baker, Christopher E.
(NASA Headquarters Washington, DC United States)
Date Acquired
May 21, 2018
Publication Date
May 7, 2018
Subject Category
Spacecraft Instrumentation And Astrionics
Report/Patent Number
NASA FS-2018-03-08-ARC
ARC-E-DAA-TN55963
Funding Number(s)
CONTRACT_GRANT: 80NSSC18M0055
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
small spacecraft
Thermal control
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