航天元器件自主可控工作推进与实施  

The Management of the Electric Coupler Internal Redundancy

作　　者：苏磊[1] 董磊[1] 刘泓[1] 熊盛阳 孙岩 Su Lei;Dong Lei;Liu Hong;Xiong Sheng-yang;Sun Yan(China Academy of Launch Vehicle Technology,Beijing,100076)

机构地区：[1]中国运载火箭技术研究院,北京100076

出　　处：《导弹与航天运载技术》2019年第2期27-30,共4页Missiles and Space Vehicles

摘　　要：为增强航天元器件自主可控水平,针对航天产品使用电子元器件的现状,分元器件的选用情况,进口元器件存在的自主可控问题,航天产品不同部位元器件自主可控风险特征,元器件自主可控推进情况存在问题等方面进行了分析。确定了航天元器件自主可控工作机制,制定了航天元器件自主可控实施方案,并提出建设全面支撑航天产品自主、安全、可控的元器件产品体系势在必行。In view of the current situation of the use of electronic components in aerospace products,the selection of components,the independent problems of imported components,the characteristics of independent risk of components in different parts and the problems of independent and controllable propulsion of components are analyzed.To enhance the level of autonomous control of aerospace components,the autonomous and controllable working mechanism of space components is determined.The implementation scheme of space components is summarized and formulated.At the same time,some measures and suggestions are put forward.

关 键 词：元器件 自主可控 措施 

分 类 号：V435[航空宇航科学与技术—航空宇航推进理论与工程]