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空间实验室低轨高压长寿命半刚性太阳电池翼技术研究
引用本文:王治易,董毅,陈建祥,杨华星,吕榕新.空间实验室低轨高压长寿命半刚性太阳电池翼技术研究[J].上海航天,2011,28(6):23-28.
作者姓名:王治易  董毅  陈建祥  杨华星  吕榕新
作者单位:上海宇航系统工程研究所,上海,201108
摘    要:介绍了国内首次使用的半刚性太阳电池翼的任务与技术指标和产品组成。给出了编织用玻璃纤维纱线制备、柔性玻璃纤维编织、半刚性基板组合工艺和低轨空间环境适应性等关键技术。阐述了研制中进行的运动学和动力学、模态、热、在轨栽荷、强度等仿真分析,以及噪声、振动、高低温展开、模态和其他试验。

关 键 词:太阳电池翼  半刚性  低轨道  高电压  仿真  试验

Technology Research of High Voltage Long Life Semi-Rigid Solar Wing with Low Orbit for Space Lab
WANG Zhi-yi,DONG Yi,CHENG Jian-xiang,YANG Hua-xing,LU Rong-xin.Technology Research of High Voltage Long Life Semi-Rigid Solar Wing with Low Orbit for Space Lab[J].Aerospace Shanghai,2011,28(6):23-28.
Authors:WANG Zhi-yi  DONG Yi  CHENG Jian-xiang  YANG Hua-xing  LU Rong-xin
Institution:WANG Zhi-yi,DONG Yi,CHENG Jian-xiang,YANG Hua-xing,LU Rong-xin(Aerospace System Engineering Shanghai,Shanghai 201108,China)
Abstract:The task,performance and composition of the semi-rigid solar array wing which was applied first time in domestic were discussed in this paper.The key technologies such as preparation of the glass fiber yarn for weaving,weaving of the soft glass fiber,technique of the semi-rigid plate combination,and environment adaptability on low orbit were given out.The simulation analysis of the kinetic and dynamic,mode,thermal,payload on-orbit and intensity in the development was descried,and so was about the experiment...
Keywords:Solar array wing  Semi-rigid  Low orbit  High voltage  Simulation  Experiment  
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