Design of space thermal environment monitoring instrument

被引：0
|
作者：
Tan, Cang-Hai [1 ]
Pan, Zeng-Fu [1 ]
Zhong, Qi [1 ]
Wu, Xiang-Jun [1 ]
机构：
[1] ISSE, CAST, Beijing 10094, China
来源：
Yuhang Xuebao/Journal of Astronautics | 2014年 / 35卷 / 05期
关键词：
Orbits - Interplanetary flight - Space research;
D O I：
10.3873/j.issn.1000-1328.2014.05.015
中图分类号：
学科分类号：
摘要：
This article presents a design of space thermal environment monitoring instrument (abbreviated as STEMI) and then analyses its performance. By contrast with standard specimen temperature and power, this instrument can measure orbit heat flux and effects of space environment on thermal coatings. This instrument is light in weight, easy to use and has real-time monitoring function. It can be applied in LEO, GEO and deep space exploration.
引用
收藏
页码：604 / 610
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