Abstract Preview
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.
General information
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Status : PublishedPublication date : 2014-02
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Edition : 1Number of pages : 17
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- ICS :
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Space systems and operations
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Materials for aerospace construction in general
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PDF + ePub | ||
Paper |
- CHF88
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