ECSS-Q-70-03A (7 April 2006)
ECSS-Q-70-03A (7 April 2006) ECSS-Q-70-03A (7 April 2006)
ECSS-Q-70-03A 7 April 2006 8 (This page is intentionally left blank)
ECSS-Q-70-03A 7 April 2006 1 Scope This Standard defines the measurements and verifications to be performed to guarantee that an anodized coating is adequate for the intended application. The rigorous requirements set by this Standard ensure the high reliability of surface treatments intended to withstand normal terrestrial conditions and the vibrational G-loads and environment imposed on spacecraft and associated equipment where surfaces require high solar absorptance, high emittance, high optical blackness, or a combination of these properties. 9
- Page 1 and 2: Space product assurance Black-anodi
- Page 3 and 4: ECSS-Q-70-03A 7 April 2006 Foreword
- Page 5 and 6: ECSS-Q-70-03A 7 April 2006 Contents
- Page 7: ECSS-Q-70-03A 7 April 2006 Introduc
- Page 11 and 12: ECSS-Q-70-03A 7 April 2006 2 Normat
- Page 13 and 14: ECSS-Q-70-03A 7 April 2006 Terms, d
- Page 15 and 16: ECSS-Q-70-03A 7 April 2006 Principl
- Page 17 and 18: ECSS-Q-70-03A 7 April 2006 Black-an
- Page 19 and 20: ECSS-Q-70-03A 7 April 2006 d. Mecha
- Page 21 and 22: 6.1 Visual inspection 6.2 Verificat
- Page 23 and 24: 7.1 General 7.2 Data 7.3 Nonconform
- Page 25 and 26: A.1 General A.2 Special utilities E
- Page 27 and 28: ECSS-Q-70-03A 7 April 2006 compleme
- Page 29 and 30: ECSS-Q-70-03A 7 April 2006 e. Steps
- Page 31 and 32: Table A-5: Dyeing with cobalt sulph
- Page 33 and 34: ECSS-Q-70-03A 7 April 2006 Bibliogr
- Page 35 and 36: ECSS Change Request / Document Impr
<strong>ECSS</strong>-Q-<strong>70</strong>-<strong>03A</strong><br />
7 <strong>April</strong> <strong>2006</strong><br />
1<br />
Scope<br />
This Standard defines the measurements and verifications to be performed to<br />
guarantee that an anodized coating is adequate for the intended application.<br />
The rigorous requirements set by this Standard ensure the high reliability of<br />
surface treatments intended to withstand normal terrestrial conditions and the<br />
vibrational G-loads and environment imposed on spacecraft and associated<br />
equipment where surfaces require high solar absorptance, high emittance, high<br />
optical blackness, or a combination of these properties.<br />
9
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