CubeSat太阳电池阵研究进展  

The Research Development of CubeSat Solar Array

作　　者：兰志成 林君毅[1] 崔新宇[1] LAN Zhicheng;LIN Junyi;CUI Xinyu(The 18th Research Institute of China Electronics Technology Group Corporation,Tianjin 300384,China)

机构地区：[1]中国电子科技集团公司第十八研究所,天津300384

出　　处：《西北工业大学学报》2020年第S01期154-160,共7页Journal of Northwestern Polytechnical University

摘　　要：立方体卫星属于微小卫星,其具有成本低、周期短等特点,因此得受到广泛应用。主要针对立方体卫星太阳能电池阵,分别从太阳电池、太阳电池基板、锁紧分离机构、太阳电池阵展开机构4个不同组成部分研究进展进行阐述,并对立方体太阳电池阵技术的发展趋势进行展望。CubeSat was applied widely as its cost was low and designed period shortly,which belongs to Picosatellite.This paper mainly described CubeSat solar array from three parts which were solar array basement,locked and released mechanism and solar array deployable device.In the end the future development of solar array technology was discussed.

关 键 词：立方体卫星 太阳电池阵 展开机构 

分 类 号：V11[航空宇航科学与技术—人机与环境工程]