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In-Space Demonstration of Spray-on Solar White PaintDiscs coated with spray-on solar white and two similar thermal control coatings were flown in low earth orbit for roughly five hours. While in orbit, the coated discs were exposed to direct sunlight and to deep space for short intervals. Measurements of disc temperatures showed that the spray-on solar white coating had the lowest absorption of sunlight. Numerical modeling was used to infer that spray-on solar white had a solar absorptance between 0.02 and 0.04 and a thermal emittance between 0.93 and 0.99, both of which are consistent with terrestrial laboratory measurements.
Document ID
20260002733
Acquisition Source
Kennedy Space Center
Document Type
Technical Memorandum (TM)
Authors
Christopher J Biagi
(Kennedy Space Center Merritt Island, United States)
Tracy L Gibson
(Southeastern Universities Research Association Washington, United States)
Madeleine J DeFilippo
(Engineering Research and Consulting Huntsville, Alabama, United States)
Date Acquired
April 3, 2026
Publication Date
April 1, 2026
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Spacecraft Design, Testing and Performance
Spacecraft Propulsion and Power
Report/Patent Number
NASA/TM-20260002733
Funding Number(s)
WBS: 114796.04.01.02.02.76
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Technical Management
Keywords
Solar White
thermal control
selective surface
cryogenic
solar reflectance
solar absorptance
thermal emissivity
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