|
[1]
|
Pan Qing, Liao Yurong, Wang Bin, et al. Operationally Responsive Space: Conception and Research Progress[M]. Beijing: National Defense Industry Press, 2010. (in Chinese) 潘清, 廖育荣, 王斌, 等. 快速响应空间概念与研究进展[M]. 北京: 国防工业出版社, 2010. |
|
[2]
|
|
|
[3]
|
Williams A D, M Eric Lyall, Derek W Hengeveld, et al. Thermal control subsystem requirements and challenges for a responsive satellite bus[C] //SPIE, 7330: 154-161. |
|
[4]
|
|
|
[5]
|
Williams A D, Palo S E. Issues and implications of the thermal control systems on the Six Day Spacecraft[C] //4th Responsive Space Conference, 2006. |
|
[6]
|
|
|
[7]
|
Galski R L, De Sousa F L, Ramou O M, et al. Spacecraft thermal design with the generalized extremal optimization algorithm[C] //Inverse Problems, Design and Optimization Symposium, 2004. |
|
[8]
|
|
|
[9]
|
Young Q E. Development of modular thermal control architecture for modular satellites [D]. US: Utah State University, 2008. |
|
[10]
|
|
|
[11]
|
Liu Jia, Li Yunze, Chang Jing, et al. A review of small satellite thermal control system[J]. Spacecraft Environment Engineering, 2011, 28(1): 77-82. (in Chinese) 刘佳, 李运泽, 常静, 等. 微小卫星热控系统的研究现状及发展趋势[J]. 航天器环境过程, 2011, 28(1): 77-82. |
|
[12]
|
|
|
[13]
|
Hou Zengqi, Hu Jingang. Spacecraft Thermal Control-Fundamentals and Application[M]. Beijing: China Science Technology Press, 2007. (in Chinese) 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. |
|
[14]
|
|
|
[15]
|
|
|
[16]
|
David G Gilmore. Spacecraft Thermal Control Handbook-Volume I: Fundamental Technologies[M]. 2nd ed. El Segundo: The Aerospace Press, 2002. |
|
[17]
|
|
|
[18]
|
Hengeveld D W. Determination of operationally responsive space(ORS) hot and cold case design orbits[C] //49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Schaumburg, 2008. |
|
[19]
|
Dou Qiang, Pang Hewei, Wei Chuanfeng, et al. The software architecture spacecraft virtual platform and its application[J]. Spacecraft Environment Engineering, 2007, 24(6): 370-373. (in Chinese) 窦强, 庞贺伟, 魏传峰, 等. 航天器虚拟热试验平台的软件架构及其应用[J]. 航天器环境工程, 2007, 24(6): 370-373. |
|
[20]
|
|
|
[21]
|
Birur Gaj. JPL Advanced thermal control technology roadmap [R]. US: Spacecraft Thermal Control Workshop, Jet Propulsion Laboratory, 2008. |
|
[22]
|
|
|
[23]
|
|
|
[24]
|
Dussinger P M, Sarraf D B, Anderson W G. Loop heat pipe for TacSat-4[C] //SPESIF, AIP Conference, 2009, 1103: 91-100. |
|
[25]
|
|
|
[26]
|
Edward Silverman, Mark Montesano. Development of an Annealed Pyrolytic Graphite material for a spacecraft electronics Packaging Payload Module[EB/OL]. NORTHOP GRUMMAN, 2004. |
|
[27]
|
Liu Dongqing, Chen Haifeng, Zheng Wenwei, et al. Application of variable infrared-emissivity materials to spacecraft thermal control[J]. Journal of National University of Defense Technology, 2012, 34(2): 145-149. (in Chinese) 刘东青, 程海峰, 郑文伟, 等. 红外发射率可变材料在航天器热控技术中的应用 [J]. 国防科技大学学报, 2012, 34(2): 145-149. |
|
[28]
|
|
|
[29]
|
Panczak T, Ring S, Welch M, et al. Thermal desktop user's manual-CAD based thermal analysis and design [Z]. US: Cullimore and Ring Technologies Inc. 2008. |
点击查看大图
下载:
