Simulated Low-Earth-Orbital Exposure of Thermal Control Materials
Author:
Affiliation:
1. The Aerospace Corporation, El Segundo, California 90245
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A33317
Reference20 articles.
1. Spectral dependence of ultraviolet-induced degradation of coatings for spacecraft thermal control
2. SteubeK. E.LinfordR. M. F. “Long Duration Exposure of Spacecraft Thermal Coatings to Simulated Near-Earth Orbital Conditions,” AIAA Paper 1971-0454, April 1971.
3. BlairP. M.Jr.PezdirtzG. F.JewellR. A. “Ultraviolet Stability of Some White Thermal Control Coatings Characterized in Vacuum,” AIAA Paper 1967-0345, April 1967.
4. An experimental study of the combined space environmental effects ona zinc-oxide - Potassium-silicate coating
5. Electron-ultraviolet radiation effects on thermal control coatings
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