ISO-16691 › Space systems - Thermal control coatings for spacecraft - General requirements

ISO-16691 - 1ST EDITION - 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.

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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