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机构地区:[1]兰州物理研究所,兰州730000
出 处:《航天器环境工程》2005年第1期41-45,49,共6页Spacecraft Environment Engineering
摘 要:文章简要介绍了同轴源原子氧装置的基本结构和工作原理;分析和计算了同轴内导体的受热状况,对内导体的结构进行了优化,使其寿命提高了近10倍,并减少了因天线氧化对真空室的污染;设计了新的试样架,试样架可同时装入4个不同试样;配置了两套紫外光源系统和一套试样光学性能原位测量系统,使装置具备了原子氧与紫外的协同效应,紫外光的波长为185~400nm,辐照度可达2~4个太阳常数;增加了光学性能测量室,试样光学性能可以原位测量。试验结果表明:优化后的原子氧装置能够模拟空间原子氧对材料的剥蚀效应。The configuration and operating process of the co-axis source atomic oxygen ground simulation facility are described in this paper.We've analyzed the thermal state of inner-conductor and optimized its structure.The life-span of the new inner-conductor is about ten times long compared with the old one,while the contamination created by the inner-conductor has been decreased greatly.We have designed a new sample tray,which four samples can be placed in.The facility is equipped with two sets of UV lights source and one suit of optical properties in-situ measurement system.The wavelength of UV lights is at the range of 200~400nm,radiation intensity is about 2~4 EUVS.Synergistic effects of atomic oxygen with UV lights can be conducted and optical properties of materials can be measured in vacuum chamber.
分 类 号:V520.2[航空宇航科学与技术—人机与环境工程] V524.3
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