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Proceedings Paper

Design method of combined protective against space environmental effects on spacecraft
Author(s): Zicai Shen; Zizheng Gong; Yigang Ding; Yuming Liu; Yenan Liu
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Paper Abstract

During its projected extended stay in LEO, spacecraft will encounter many environmental factors including energetic particles, ultraviolet radiation, atomic oxygen, and space debris and meteoroids, together with some induced environments such as contamination and discharging. These space environments and their effects have threat to the reliability and lifetime of spacecraft. So, it is important to give a combined design against the threat from space environments and their effects. The space environments and effects are reviewed in this paper firstly. Secondly, the design process and method against space environments are discussed. At last, some advices about protective structure and materials are proposed.

Paper Details

Date Published: 26 January 2016
PDF: 5 pages
Proc. SPIE 9796, Selected Papers of the Photoelectronic Technology Committee Conferences held November 2015, 979615 (26 January 2016); doi: 10.1117/12.2228609
Show Author Affiliations
Zicai Shen, Beijing Institute of Spacecraft Environment Engineering (China)
Zizheng Gong, Beijing Institute of Spacecraft Environment Engineering (China)
Yigang Ding, Beijing Institute of Spacecraft Environment Engineering (China)
Yuming Liu, Beijing Institute of Spacecraft Environment Engineering (China)
Yenan Liu, Beijing Institute of Spacecraft Environment Engineering (China)


Published in SPIE Proceedings Vol. 9796:
Selected Papers of the Photoelectronic Technology Committee Conferences held November 2015
Weimin Bao; Yueguang Lv, Editor(s)

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