FIELD: protection of elements of structures and articles of rocket and space equipment. SUBSTANCE: proposed coating includes layer manufactured from temperature controlling material and made fast to coated surface with the use of sublayer produced from current conductive material which thickness on coated surface amounts to not more than 30 μ. Its developed surface made in the form of recesses and protrusions whose height difference is from 30 to 200 μ faces temperature controlling material. Temperature controlling material is located in recesses of current conductive material. EFFECT: coating provides for protection of articles from electrostatic charges and ensures heat conditions of their usage. 1 dwg
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Authors
Dates
1999-02-20—Published
1998-03-31—Filed