首页> 外文期刊>Journal of Spacecraft and Rockets >Inorganic White Thermal-Control Coatings for Extreme Space Environments
【24h】

Inorganic White Thermal-Control Coatings for Extreme Space Environments

机译:适用于极端空间环境的无机白热控制涂料

获取原文
获取原文并翻译 | 示例
获取外文期刊封面目录资料

摘要

White paints and clear anodizing are often used as thermal-control coatings. Inorganic white ceramic coating on AA2219 alloy prepared using novel Keronite plasma-electrolytic-oxidation technology was used in this study for the BepiColombo mission. The Keronite coating on a high copper-containing 2219 aluminum alloy was investigated in terms of its resistance to environmental exposures, such as corrosion, humidity, and high-temperature (400 degrees C) UV/VUV radiation. The coating was characterized in terms of its microstructure, porosity, and adhesion, and their relations to the overall thermooptical performance and space suitability. Optical reflectivity, spectrophotometer color, solar absorptance, and hemispherical emittance have been measured and compared against that of currently used white silicone paint. The Keronite white coating has been shown to offer thermooptical characteristics acceptable as a space thermal-control material, while offering all the added benefits of 1) inorganic ceramic coating with extremely good adhesion, 2) environmentally friendly process with no toxic substances and heavy metals, 3) capability to coat shapes with complex geometries and non-line-of-sight areas, and 4) resistance to harsh space environment. The ceramic white coating has now been applied on Mercury Planetary Orbiter solar-array thermal shields.
机译:白色涂料和透明阳极氧化通常用作热控涂料。在这项研究中,使用新颖的Keronite等离子体电解氧化技术在AA2219合金上制备了无机白色陶瓷涂层,以完成BepiColombo任务。对高含铜2219铝合金上的Keronite涂层进行了耐环境暴露(例如腐蚀,潮湿和高温(400摄氏度)UV / VUV辐射)耐受性研究。该涂层的特征在于其微观结构,孔隙率和附着力,以及它们与整体热光学性能和空间适用性的关系。测量了光反射率,分光光度计的颜色,日光吸收率和半球形发射率,并将其与当前使用的白色有机硅涂料进行了比较。事实证明,Keronite白色涂层具有作为空间温度控制材料可接受的热光学特性,同时具有以下所有附加优点:1)无机陶瓷涂层具有极佳的附着力; 2)环保工艺,无毒物质和重金属, 3)能够涂覆具有复杂几何形状和非视线区域的形状,以及4)抵抗恶劣的太空环境。陶瓷白色涂层现已应用于Mercury Planetary Orbiter太阳电池阵列隔热屏。

著录项

  • 来源
    《Journal of Spacecraft and Rockets》 |2016年第6期|1061-1067|共7页
  • 作者单位

    Keronite Int Ltd, Haverhill CB9 8PJ, England|Univ Leeds, Leeds, W Yorkshire, England;

    Airbus DS GmbH, Mat & Proc Dept, D-81663 Ottobrunn, Germany;

    Dokuz Eylul Univ, Met & Mat Engn Dept, TR-35160 Buca Izmir, Turkey;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号