
ISO 16691:2014
ISO 16691:2014 Space systems – Thermal control coatings for spacecraft – General requirements
CDN $173.00
Description
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.
Edition
1
Published Date
2014-02-10
Status
PUBLISHED
Pages
17
Format 
Secure PDF
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Abstract
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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