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Low Earth orbit durability of protected silicone for refractive photovoltaic concentrator arrays
Author(s) -
Kim K. de Groh,
Timothy A. McCollum
Publication year - 1995
Publication title -
journal of spacecraft and rockets
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.758
H-Index - 79
eISSN - 1533-6794
pISSN - 0022-4650
DOI - 10.2514/3.26581
Subject(s) - spacecraft , aerospace engineering , missile , concentrator , low earth orbit , photovoltaic system , durability , space (punctuation) , orbit (dynamics) , space environment , spacecraft design , systems engineering , geocentric orbit , engineering , mechanical engineering , computer science , satellite , physics , electrical engineering , database , geophysics , operating system
Photovoltaic power systems with novel refractive silicone solar concentrators are being developed for use in low Earth orbit (LEO). Because of the vulnerability of silicones to atomic oxygen and ultraviolet radiation, these lenses are coated with a multilayer metal oxide protective coating. The objective of this work was to evaluate the effects of atomic oxygen and thermal exposures on multilayer coated silicone. Samples were exposed to high-fluence ground-laboratory and low-fluence in-space atomic oxygen. Ground testing resulted in decreases in both total and specular transmittance, while in-space exposure resulted in only small decreases in specular transmittance. A contamination film, attributed to exposed silicone at coating crack sites, was found to cause transmittance decreases during ground testing. Propagation of coating cracks was found to be the result of sample heating during exposure. The potential for silicone exposure, with the resulting degradation of optical properties from silicone contamination, indicates that this multilayer coated silicone is not durable for LEO space applications where thermal exposures will cause coating crack development and propagation.

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