| 航天器系统设计的可靠性准则 |
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| 引用本文： | 谭维炽,张伍. 航天器系统设计的可靠性准则[J]. 航天器工程, 2012, 21(2): 1-5 |
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| 作者姓名： | 谭维炽 张伍 |
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| 作者单位： | 1. 中国空间技术研究院,北京,100094
2. 北京空间飞行器总体设计部,北京,100094 |
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| 摘 要： | 在对大量航天器工程案例分析的基础上,提炼出10条航天器系统（总体）设计的可靠性准则。遵循这些设计准则,将有利于航天器从系统级避免许多故障,或者消除故障对系统的影响,在阐述每条准则时,列举了一个或数个案例。
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| 关 键 词： | 航天器 系统设计 可靠性准则 |
Reliability Rules for Spacecraft System Design |
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| TAN Weichi,ZHANG Wu. Reliability Rules for Spacecraft System Design[J]. Spacecraft Engineering, 2012, 21(2): 1-5 |
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| Authors: | TAN Weichi ZHANG Wu |
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| Affiliation: | 1 China Academy of Space Technology,Beijing 100094,China)(2 Beijing Institute of Spacecraft System Engineering,Beijing 100094,China) |
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| Abstract: | Based on analyzing of the engineering cases about spacecraft,10 reliability rules for spacecraft system design are proposed in this paper.Followed these rules,some system faults will be avoided,or some effect of faults on the system will be eliminated.One or several cases are particularized. |
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| Keywords: | spacecraft system design reliability rule |
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