TEMPERATURE CONTROL COAT Russian patent published in 2008 - IPC C09D5/24 C09D133/08 

FIELD: temperature control coats applied on external surface of spacecraft for maintenance of definite thermal conditions.

SUBSTANCE: proposed temperature control coat is made from composition including amide-containing acryl resin in the amount of 1.0-1.1 parts by mass which is used as binder; mixture of xylol and butyl alcohol used as solvent; black heat-resistant pigment in the amount of 1.86-1.9 parts by mass which is used as filler, carbonylic nickel in the amount of 0.30-0.40 parts by mass at content of nickel of 99.5-99.9% and soot - commercial carbon in the amount of 0.03-0.04 parts by mass. Proposed coat has specific volumetric electric resistance not exceeding ρv≤7·10³ ohms·m.

EFFECT: enhanced efficiency; low level of gas evolution.