SPACECRAFT THERMAL BLANKET Russian patent published in 2016 - IPC B64G1/58 

Abstract RU 2587740 C2

FIELD: astronautics.

SUBSTANCE: invention relates to heat insulation of spacecraft. Spacecraft thermal blanket consists of alternating layers formed non-flat polymer film with single or double-sided sputtering of metal, for example aluminium, and polymer network on which can be applied hot-melt adhesive. Polymers used as for making films and for making net include polyester, polyimide, aramid, arimid.

EFFECT: low heat conductivity and total weight of heat insulation.

1 cl, 6 dwg, 2 tbl

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RU 2 587 740 C2

Authors

Aristov Vasilij Fedorovich

Dates

2016-06-20Published

2013-06-11Filed