ISO 16691:2014 defines general requirements for thermal control coatings (TCC) that are applied on metallic and/or non-metallic surfaces of spacecraft and payloads in order to provide the following thermo-optical properties: αs: solar absorptance; ε: emittance.
The function of TCC is to reduce external heat absorption and/or to regulate radiant heat exchange between on-board equipment on spacecraft.
Status: PublishedPublication date: 2014-02
Edition: 1Number of pages: 17
Technical Committee: ISO/TC 20/SC 14 Space systems and operations
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