FIELD: process engineering.
SUBSTANCE: invention relates to application of electrically conducting coating on outer surface of spacecraft optoelectronic device. Proposed method consists in that assembled and painted from inside sun blade is fitted on base running in two axes in vacuum chamber. Coating with different current conductivity is deposited by evaporation in vacuum chamber.
EFFECT: electrically conducting coating on outer surface of spacecraft optoelectronic device.
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Authors
Dates
2014-08-27—Published
2012-12-13—Filed