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Thermal design of star sensor assembly
Jiang F.; Wang Z.; Chen L.; Wu Q.; Guo L.
2014
发表期刊Hongwai yu Jiguang Gongcheng/Infrared and Laser Engineering
ISSNISBN/10072276
卷号43期号:11页码:3740-3745
摘要Based on the structure character and mission requirements of star sensors used by high detectivity satellites, thermal design of star sensor assembly was accomplished by combining thermal simulation analysis and thermal balance test. Firstly, the temperature target of the bracket of the star sensors was determined by the thermal transformation analysis. Then according to the orbit parameters and the positions of star sensors, the incident space heat fluxes of three star sensors were computed. Besides the fluxes, internal heat sources of star sensors and degradation of MLI were also considered to complete the design. Both the passive thermal control and the active thermal control were applied. The simulation analysis indicates that the temperatures of the assembly was between 17.0 to 19.1. Finally, the thermal design was examined by thermal balance test and temperature test in orbit. The results of thermal balance test show that the temperatures of the assembly are between 17.3 to 18.7 and the remote data show that the temperatures are between 16.0 to 19.1. Both the data indicate that the temperatures of the assembly are between 183 and the thermal design is valid and reasonable which can meet the mission requirements.
收录类别EI
语种中文
文献类型期刊论文
条目标识符http://ir.ciomp.ac.cn/handle/181722/44467
专题中科院长春光机所知识产出
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GB/T 7714
Jiang F.,Wang Z.,Chen L.,et al. Thermal design of star sensor assembly[J]. Hongwai yu Jiguang Gongcheng/Infrared and Laser Engineering,2014,43(11):3740-3745.
APA Jiang F.,Wang Z.,Chen L.,Wu Q.,&Guo L..(2014).Thermal design of star sensor assembly.Hongwai yu Jiguang Gongcheng/Infrared and Laser Engineering,43(11),3740-3745.
MLA Jiang F.,et al."Thermal design of star sensor assembly".Hongwai yu Jiguang Gongcheng/Infrared and Laser Engineering 43.11(2014):3740-3745.
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