Abstract

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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.


General information 

  • Status
     : Published
    Publication date
     : 2014-02
  • Edition
     : 1
    Number of pages
     : 17
  • Technical Committee
     : ISO/TC 20/SC 14 Space systems and operations
  • ICS
     :
    49.140 Space systems and operations
    49.025.01 Materials for aerospace construction in general

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