FIELD: physics.
SUBSTANCE: temperature-control coating in spacecraft structures is used on the surface of optical devices, surveillance systems and radiators of active systems. The temperature-control coating is made from a composition containing, as a binding agent, a solution of an amide-containing acrylic resin in solvent mixture of xylene and butyl alcohol in ratio of 4:1, as filler - black heat-resistant pigment, carbonyl nickel and additionally iron oxide nanoparticles.
EFFECT: improved optical coefficients of the temperature-control coating and obtaining the required temperature-control coating.
1 tbl, 6 ex
Title | Year | Author | Number |
---|---|---|---|
ENAMEL COMPOSITION FOR MAKING THERMOREGULATING COATING | 2017 |
|
RU2683752C1 |
TEMPERATURE CONTROL COAT | 2006 |
|
RU2315794C1 |
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|
RU2283332C1 |
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RU2560396C1 |
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RU2443738C1 |
SOLAR REFLECTOR CLASS TEMPERATURE-CONTROLLED COATING COMPOSITION | 2008 |
|
RU2401852C2 |
THERMOSTATIC COATING OF "SOLAR REFLECTOR" CLASS | 2009 |
|
RU2421490C1 |
RADIATION PROTECTING TEMPERATURE-CONTROLLED COATING FOR SPACECRAFTS | 2014 |
|
RU2554183C1 |
METHOD OF PRODUCING ENAMEL COMPOSITION FOR TEMPERATURE-CONTROL COATINGS | 2014 |
|
RU2563281C1 |
ADHESIVE POLYMER COMPOSITION POSSESSING MAGNETIC PROPERTIES | 2002 |
|
RU2225425C1 |
Authors
Dates
2014-07-27—Published
2013-01-22—Filed