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温控白漆原子氧、紫外综合环境效应退化影响初步研究
引用本文:温控白漆原子氧、紫外综合环境效应退化影响初步研究[J]. 航天器环境工程, 2003, 20(4): 19-24.
作者姓名:童靖宇  王吉辉  李金洪
作者单位:北京卫星环境工程研究所,北京,100029;北京卫星环境工程研究所,北京,100029;北京卫星环境工程研究所,北京,100029
摘    要:文章主要介绍了对S781、SR107-ZK两种国产温控白漆进行地面单一原子氧环境、原子氧/紫外综合环境效应模拟试验的情况.试验条件为短期环境暴露试验,原子氧积分通量、紫外辐照积分量按照STS-8轨道条件设计.采用SEM、XPS、光谱计、微量天平等对试验前后的样品进行了表面形貌、表面成分、太阳吸收率、质损分析,对这两种国产温控白漆原子氧、紫外环境效应退化规律有了初步认识.

关 键 词:温控漆  原子氧  紫外
文章编号:(2003)04-0019-06
收稿时间:2003-07-15
修稿时间:2003-07-15

PRELIMINARY RESEARCH ON DEGRADATION OF THE THERMAL CONTROL PAINTS IN AO/UV ENVIRIONMENT
PRELIMINARY RESEARCH ON DEGRADATION OF THE THERMAL CONTROL PAINTS IN AO/UV ENVIRIONMENT[J]. Spacecraft Environment Engineering, 2003, 20(4): 19-24.
Authors:TONG Jing-yu  WANG Ji-hui  Li Jin-hong
Abstract:Some experiments of AO effects and AO/UV synergistic effects on two thermal control paints,S781 and SR107-ZK,have been completed at the Beijing Institute of Spacecraft Environment Engineering.The test samples were exposed to the simulated space environment,same as STS-8,for short duration.The morphology,mass loss,solar absorptivity and composition of specimens were analyzed by SEM,microbalance,spectrophotometer,and XPS before and after exposure. The degradation of the two paints has been investigated prelimilarily.
Keywords:thermal control paint  atomic oxygen  ultraviolet
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