ISO 16691:2014

Space systems — Thermal control coatings for spacecraft — General requirements

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.

SDO:

ISO

Language:

English

ICS Codes:

49.025.01; 49.140

Status:

Published

Publish date:

2014-02-09

Standard Number:

ISO 16691:2014