立方体卫星太阳翼技术综述  

Overview of Solar Wing for CubeSat

作　　者：任守志[1] 刘颖[1] 王举[1] 黄传平[1] 刘少锋[1] 马静雅[1] 周志清[1] 

机构地区：[1]北京空间飞行器总体设计部,北京100094

出　　处：《航天器工程》2015年第2期109-118,共10页Spacecraft Engineering

摘　　要：调研了国外不同类型立方体卫星(CubeSat)的太阳翼技术,并从展开维度及展开次数的角度进行了分类,然后对CubeSat太阳翼的太阳电池板、压紧释放机构及展开机构等典型部件进行详细介绍,对不同类型的部件技术进行了对比,通过对比,给出了CubeSat太阳翼在研制体系建设、部件技术、搭载验证等方面的发展建议,可为后续研究提供参考。This paper investigates different kinds of solar wing on CubeSats, makes a classification of them in the view of dimension and times of deployment. It presents a detailed introduction of their typical components--solar panel, hold-down and release mechanism and deployment mecha- nism. The paper also compares different types of the components and gives specific advice to con- cerned researchers on development system, parts design and flight test of the CubeSat solar wings. The results can he as a reference for the future research.

关 键 词：立方体卫星 展开式 太阳翼 

分 类 号：V442[航空宇航科学与技术—飞行器设计]