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Contamination sensitivity of typical mirror coatings - A parametric studyContamination budgeting for space optical systems basically starts at understanding the sensitivity of component performance, e.g. mirror reflectance, window transmittance, etc., to surface deposits. To evaluate contamination sensitivity for mirror coatings, eight types representative of those used in the vacuum ultraviolet, visible, and infrared were modeled assuming that the contaminant is uniformly deposited on the mirror surface. Parametric studies over a range of complex refractive indices combined with an examination of optical data available for several organic materials suggested division of the contaminant layer index into three categories, N = 1.5 + 0.1i, N = 1.5 + 0.5i, and N = 1.5 + 2.0i. Contaminant thickness sensitivity curves were then calculated for each of the selected mirror coatings. For comparative purposes, critical thicknesses for each type were extracted, assuming a reflectance loss of 10 percent was allowable. Critical thicknesses ranged from about 10 A to 1000 A depending on the specifics of coating design and spectral region.
Document ID
19840045673
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Osantowski, J. F.
(NASA Goddard Space Flight Center Space Technology Div., Greenbelt, MD, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1983
Subject Category
Optics
Accession Number
84A28460
Distribution Limits
Public
Copyright
Other

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