CHENG De,WANG Jing-run,QIN Ye-shen,ZHAO Lian-jing,GUO Zhong-zeng,WANG Xu-guang,BAI Jing-ying,LI Si-zhen.Properties and Stability in Space Environment of BN-1:An Ultra-high Absorption Conductive Matting Coating[J],50(11):195-201
Properties and Stability in Space Environment of BN-1:An Ultra-high Absorption Conductive Matting Coating
Received:November 26, 2020  Revised:May 13, 2021
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DOI:10.16490/j.cnki.issn.1001-3660.2021.11.019
KeyWord:BN-1  high absorption  conductivity  extinction performance  coating  space environment
                       
AuthorInstitution
CHENG De Beijing Spacecrafts, Beijing , China
WANG Jing-run Beijing Spacecrafts, Beijing , China
QIN Ye-shen Beijing Spacecrafts, Beijing , China
ZHAO Lian-jing Beijing Spacecrafts, Beijing , China
GUO Zhong-zeng Beijing Spacecrafts, Beijing , China
WANG Xu-guang Beijing Spacecrafts, Beijing , China
BAI Jing-ying Beijing Spacecrafts, Beijing , China
LI Si-zhen Beijing Spacecrafts, Beijing , China
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Abstract:
      The microstructure, conductivity and absorptivity of an ultra-high absorption conductive matting coating (BN-1 coating) and the influence of space irradiation environment on it were studied to evaluate whether the coating meet the requirements of long-life space optical component. Firstly, the micro morphology, element composition, contact resistance, solar absorption ratio (αs) of the BN-1 coating were tested to investigate the conductivity and extinction properties of the coating. The structural basis of the coating extinction performance was analyzed on this basis. Then, the BN-1 coating was irradiated with atomic oxygen dose of 2.0×1021 atoms/cm2 and vacuum-ultraviolet dose of 5000 ESH respectively. The effect of space simulated irradiation environment on BN-1 coating is analyzed through the test results and the stability of BN-1 coating against space environment was studied. Micro-nanometer holes are evenly distributed on the surface of the BN-1 coating which was called light trap structure, leading to the excellent conductivity and absorptivity of the BN-1 coating. The contact resistance is less than 5 mΩ, and the solar absorption ratio (αs) is greater than 0.98. After AO exposure, the solar absorption ratio (αs) of the BN-1 coating decreased by 0.0049 and the change value is less than 0.01. It has good resistance to atomic sunlight irradiation. After VUV irradiation, the solar absorption ratio (αs) of the BN-1 coating increased by 0.0009 and the change value was less than 0.01. It has good resistance to vacuum ultraviolet radiation. BN-1 coating has excellent conductivity and extinction performance. After AO and VUV simulated irradiation, BN-1 coating αs change is small and has good space irradiation resistance, which can meet the long-life service requirements of space optical components such as star sensor and space camera.
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