期刊文献+

原子氧与紫外综合辐照下Kapton/Al结构变化

Effect of atomic oxygen and ultraviolet on surface structure and composition of Kapton/Al film
在线阅读 下载PDF
导出
摘要 在激光源原子氧地面模拟设备中对Kapton/Al薄膜二次表面镜进行了原子氧与紫外综合辐照实验,研究了Kapton/Al薄膜质量及太阳吸收比的变化,重点关注了实验前后Kapton/Al薄膜表面结构及成份的改变。结果表明:Kapton/Al薄膜二次表面镜的质量随辐照时间的增加逐渐减小,太阳吸收比的变化趋势与之相反,随辐照时间的增加逐渐增大;综合辐照后Kapton/Al薄膜表面主要官能团数量呈下降趋势;综合辐照过程中材料表面C-C键、C-N键的破坏及在原子氧和紫外环境中重新结合成新的化学结构是造成Kapton/Al薄膜性能退化的主要微观机制,气体小分子的挥发是造成Kapton/Al薄膜质量损失的主要原因。 Atomic oxygen (AO), near ultraviolet (NUV) and vacuum ultraviolet (VUV) irradiation test of Kapton/A1 sec-ond surface mirror film was conducted using laser induced AO simulation faeility the mass, solar ahsorptance, surface structureand composition were investigated. The results indicate that the mass of Kapton/A1 film is decreased with increasing irradiationtime, but the solar absorptance displays entirely different trend, which is increased with increasing irradiation time. After irradia-tion, the quantity of the main functional groups in Kapton/A1 film surface presents downtrend basically. The breakage of C--Cand C--N bonds and new chemical bond creation in Kapton/A1 film surface are considered mechanisms of the degradation, and gasmolecule volatilization leads to the mass loss of Kapton/A1 film.
出处 《强激光与粒子束》 EI CAS CSCD 北大核心 2015年第12期196-202,共7页 High Power Laser and Particle Beams
基金 国家自然科学基金项目(51301005 41304147 21277014) 总装预研基金项目
关键词 原子氧 紫外 辐照 Kapton/Al 表面结构 atomic oxygen ultraviolet irradiation Kapton/A1 surface structure
作者简介 姜海富,男,博士,从事航天器空间环境效应研究
  • 相关文献

参考文献17

  • 1郑阔海,李中华,王敬宜,赵琳.低地球轨道航天器不同攻角原子氧通量密度计算模型[J].宇航学报,2010,31(7):1855-1863. 被引量:9
  • 2Mundati N D A, Srivastava A K,Toyoda K, et al. Influence of atomic oxygen exposure on surface resistivity of silicon doped polyimide af-fecting spacecraft charging[J]. Vacuum , 2014, 105 : 11-16.
  • 3沈嘉年,何砚发,周龙江,李美栓.高通量中性原子氧束流的发生与控制[J].强激光与粒子束,2001,13(2):228-232. 被引量:4
  • 4Tagawa M, Yokota K. Atomic oxygen-induced polymer degradation phenomena in simulated LEO space environment: How do polymers re-act in a complicated space environment. [J]. Acta Astronautica , 2008, 62:203-211.
  • 5田聪,成来飞,栾新刚.C/C复合材料在原子氧辐照下的结构性能演变[J].无机材料学报,2013,28(8):853-858. 被引量:4
  • 6李国禄,王海斗,徐滨士,马国政,张森.空间原子氧辐照对电刷镀Ni/MoS_2-C镀层组织结构及摩擦学性能的影响[J].材料工程,2014,42(2):24-28. 被引量:8
  • 7Misak H E, Sabelkin V,Mall S,et al. Thermal fatigue and hypothermal atomic oxygen exposure behavior of carbon nanotube wire[J].Carbon,2013,57:42-49.
  • 8Hu L F,Li M S,Xu C H,et al. A polysilazane coating protecting polyimide from atomic oxygen and vacuum ultraviolet radiation erosion[J]. Surface Coatings Technology , 2009, 203:3338-3343.
  • 9Shuvalov V A, Pis^mennyi N I,Kochubei G S,et al. The mass loss of spacecraft polyimide films under the action of atomic oxygen and vac-uum ultraviolet radiation[J], Cosmic Research , 2014, 52(2) . 99-105.
  • 10Liu X F,Wang L P,Xue Q J,et al. High vacuum tribological performance of DLC-based solid-liquid lubricating coatings: influence of a-tomic oxygen and ultraviolet irradiation[J], Tribology International, 2013,60:36-44.

二级参考文献50

共引文献41

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部