In the design of spacecraft for proper thermal balance, accurate information on the long-term optical behavior of the spacecraft outer skin materials is necessary. A phenomenological model for such behavior is given. The underlying principles are explained and some examples are given of the model's fit to actual measurements under simulated Earth-orbit conditions. Comments are given on the applicability of the model to materials testing and thermal modelling.
Mathematical modelling of solar ultraviolet radiation induced optical degradation in anodized aluminum
01.01.1986
Aufsatz (Konferenz)
Keine Angabe
Englisch
ANODIZED ALUMINUM AUTOMOTIVE PARTS
SAE Technical Papers | 1985
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|ANODIZED ALUMINUM AUTOMOTIVE PARTS
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