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Optical solar reflector thermal-control coating on satellite solar panel surface and preparation method of coating

A secondary surface mirror and substrate surface technology, applied in the surface pretreatment of the bonding method, coating, bonding method, etc., can solve the problems of unverified adhesion, increased difficulty in squeegeeing, uneven unevenness, and achieve Strong implementability, good adhesion, good adhesion effect

Inactive Publication Date: 2019-05-03
SHANGHAI INST OF SATELLITE EQUIP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] There are three difficulties in pasting the OSR film on the surface of the polyimide film of the satellite solar substrate: 1) The surface of the substrate is uneven, and the surface of the polyimide film is smooth, which makes it more difficult to scrape the glue, and the adhesion needs to be verified

Method used

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  • Optical solar reflector thermal-control coating on satellite solar panel surface and preparation method of coating
  • Optical solar reflector thermal-control coating on satellite solar panel surface and preparation method of coating
  • Optical solar reflector thermal-control coating on satellite solar panel surface and preparation method of coating

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Embodiment Construction

[0037] The present invention will be described in detail below in conjunction with specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be noted that those skilled in the art can make several changes and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention.

[0038] A thermal control coating for a glass-type secondary surface mirror on the surface of a satellite solar substrate, comprising: an OSR sheet, conductive glue and a surface treatment agent;

[0039] The conductive adhesive is an adhesive mixed with component A, component B and silver powder in a predetermined ratio;

[0040] The surface treatment agent includes KH550 silane coupling agent.

[0041] Preferably, component A and component B include:

[0042] The components of 601 adhesive, in which ...

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Abstract

The invention provides an optical solar reflector thermal-control coating on the satellite solar panel surface and a preparation method of the coating. The coating comprises the following components:an optical solar reflector, a conductive adhesive and a surface treatment agent, wherein the conductive adhesive is an adhesive formed by mixing an A component, a B component and silver powder according to a predetermined ratio, and the surface treatment agent includes a KH550 silane coupling agent. The coating provided by the invention has better coating electrical conductivity on the basis thatgood thermal control performance (solar absorption ratio and hemispherical emissivity) of the coating is ensured, and the coating has very good adhesion after subjected to surface treatment.

Description

technical field [0001] The invention relates to the technical field of aircraft thermal control materials, in particular to a thermal control coating for a glass-type secondary surface mirror on the surface of a satellite solar substrate and a preparation method thereof. Background technique [0002] Anti-static cerium glass silver-plated secondary surface mirror, also known as optical solar reflector, or "OSR" for short, is one of the most ideal thermal control materials for long-life satellites. OSR is pasted on the outer surface of the satellite to effectively control the surface of the satellite. temperature, to ensure the normal operation of the instruments and equipment on the spacecraft, and to ensure that the spacecraft can complete the specified tasks during the design life. Anti-static cerium glass silver-plated secondary surface mirror is used as a special thermal control material in the thermal control field of spacecraft. Therefore, it is more and more widely u...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): C09D5/32C09D5/00C09D5/24C09J5/00C09J5/02C09J9/02C09J201/00
Inventor 隋微微陈砚朋孙敬文任晓雯
Owner SHANGHAI INST OF SATELLITE EQUIP
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