Dynamical thermal analysis of microchannel cooling system for in-orbit nano-satellite

[1] 侯增祺,胡金刚.航天器热控制技术——原理及其应用[M].北京: 中国科学技术出版社,2007:113-115 Hou Zengqi, Hu Jingang. Thermal control—theory and applications [M]. Beijing: Chinese Technology Press, 2007:113-115(in Chinese) [2] Gilmore D G. Spacecraft thermal control handbook [M].Second Edition.E1 Segundo, California: The Aerospace Corporation Press, 2002:405-415 [3] Volodymyr B. Micro-satellites thermal control-concepts and components[J]. Acta Astronautica, 2005, 56: 161-170 [4] Paris A D, Birur G C, Green A A. Development of MEMS microchannel heat sinks for micro/nano spacecraft thermal control . IMECE2002-34293,2002 [5] Birur G C, Sur T W, Paris A D, et al. Micro/nano spacecraft thermal control using a MEMS-based pumped liquid cooling system //Carlos H M, Holger B.SPIE International Symposium on Micromachining and Microfabrication. USA: Microfluidics and BioMEMS, 2001:196-205 [6] 李运泽,魏传锋,袁领双,等.卫星热控系统的动态特性建模与仿真[J].北京航空航天大学学报,2005,31(3):372-374 Li Yunze, Wei Chuanfeng, Yuan Lingshuang, et al. Dynamical modeling and simulation of satellite thermal control system[J]. Journal of Beijing University of Aeronautics and Astronautics, 2005,31(3):372-374(in Chinese) [7] 李运泽,宁献文,王晓明,等.纳卫星轨道热环境仿真分析[J].系统仿真学报,2007,19(14):3166-3168 Li Yunze, Ning Xianwen, Wang Xiaoming, et al. Simulation analysis of nano-satellite-s orbital thermal environment[J]. Journal of System Simulation, 2007,19(14):3166-3168(in Chinese)