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Electrodynamic Dust Shield for Active Dust Mitigation of Thermal RadiatorsThis project sought to investigate whether the Electrodynamic Dust Shield (EDS) would work with various thermal control coatings (TCC) to remove dust off the TCC. Keeping surfaces dust free is essential for thermal radiators as the dust acts as both a blackbody and a thermal insulator so it will absorb more sunlight and prevent the radiator from radiating heat. The lack of heat rejection on dusty surfaces causes the radiator to be oversized and potentially cause catastrophic system failure due to overheating. With an EDS integrated into the radiator system, dust impacts can be mitigated by removing the dust off the surface using electric fields. This project tested dust removal, solar absorptance, emittance, and limited thermal vacuum with a TCC on an EDS which is bonded to an aluminum plate acting like a radiator. The results of various coatings suggests that the EDS can work with insulative TCC in high vacuum for removing dust, and that after removing dust, the solar absorptance can be restored to within 5-10% of its original value when the EDS works properly. More work is necessary to determine how the EDS impacts the emittance of the whole radiator system and bonding between the different layers needs to be investigated to withstand temperature cycling of the moon without delamination occurring.
Document ID
20240000514
Acquisition Source
Kennedy Space Center
Document Type
Other - Report Summary
Authors
Krystal Acosta
(Kennedy Space Center Merritt Island, Florida, United States)
Joseph Toth
(Kennedy Space Center Merritt Island, Florida, United States)
Tracy Gibson
(Engineering Research and Consulting Merritt Island, Florida, United States)
Date Acquired
January 12, 2024
Publication Date
January 31, 2024
Report/Patent Number
CIF 22-3
Funding Number(s)
WBS: 295640
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Technical Management
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