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CubeSat Form Factor Thermal Control LouversThermal control louvers for CubeSats or small spacecraft may include a plurality of springs attached to a back panel of the thermal control louvers. The thermal control louvers may also include a front panel, which includes at least two end panels interlocked with one or more middle panels. The front panel may secure the springs, shafts, and flaps to the back panel.
Document ID
20180002488
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Evans, Allison L.
Date Acquired
April 23, 2018
Publication Date
January 9, 2018
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
Patent Number: US-Patent-9,862,507
Patent Application Number: US-Patent-Appl-SN-14/867,896
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-9,862,507
Patent Application
US-Patent-Appl-SN-14/867,896

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