ISO-16691 › Space systems - Thermal control coatings for spacecraft - General requirements
ISO-16691
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1ST EDITION
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CURRENT
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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.
To find similar documents by classification:
49.025.01 (Materials for aerospace construction in general)
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Document Number
ISO 16691:2014
Revision Level
1ST EDITION
Status
Current
Publication Date
Feb. 15, 2014
Committee Number
ISO/TC 20/SC 14