BS ISO 16691:2014
Current
The latest, up-to-date edition.
Space systems. Thermal control coatings for spacecraft. General requirements
Hardcopy , PDF
English
28-02-2014
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Foreword
Introduction
1 Scope
2 Normative references
3 Terms, definitions, and abbreviated terms
4 General
5 Selection
6 Test methods for TCC
7 Requirements for application
8 Safety requirements for TCC application
9 Identification
10 Protectors
11 Packing
12 Production program of quality assurance
13 Changes and revisions
Annex A (informative) - General properties
of TCC-I and TCC-II
Bibliography
Describes 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: - alpha s: solar absorptance; - varepsilon: emittance.
| Committee |
ACE/68
|
| DevelopmentNote |
Supersedes 13/30269751 DC. (02/2014)
|
| DocumentType |
Standard
|
| Pages |
28
|
| PublisherName |
British Standards Institution
|
| Status |
Current
|
| Supersedes |
This International Standard 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.
| Standards | Relationship |
| ISO 16691:2014 | Identical |
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