ISO 16691:2014

Space systems — Thermal control coatings for spacecraft — General requirements

OVERVIEW

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: as: solar absorptance; e: emittance.

The function of TCC is to reduce external heat absorption and/or to regulate radiant heat exchange between on-board equipment on spacecraft.

COMMENTS

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PRODUCT DETAILS

Status Current
Edition 2014
No. of Pages 17
ICS Classification 49.025.01 Materials for aerospace construction in general
49.140 Space systems and operations
Committee ISO/TC 20/SC 14
Available for Purchase For sale in Singapore only
Adoption ISO