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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: 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.
| Author | ISO/TC 20/SC 14 Space systems and operations |
|---|---|
| Editor | ISO |
| Document type | Standard |
| Format | Paper |
| Edition | 1 |
| ICS | 49.140 : Space systems and operations |
| Number of pages | 17 |
| Weight(kg.) | 0.1289 |
| Year | 2014 |
| Country | Switzerland |