Publikationsdatum:
2019-06-27
Beschreibung:
Conductive transparent coatings applied to the dielectric surfaces of a spacecraft offer the possibility of distributing charge uniformly over the entire spacecraft surface. Optical and electrical measurements of such a coating as a function of temperature are described. These results are used in considering the impact of a conductive coating on the absorptance of thermal control mirrors and on the transmittance of solar cell cover glass, which can be improved by the application of an antireflection coating.
Schlagwort(e):
RESEARCH AND SUPPORT FACILITIES (AIR)
Materialart:
PAPER-17
,
NASA. Goddard Space Flight Center 8th Conf. on Space Simulation; p 187-193
Format:
text
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