红外技术, 2011, 33 (5): 305, 网络出版: 2011-06-24
基于航天器表面涂层材料的热设计分析及应用
Thermal Design Analysis and Application on the Surface Coating Materials of Spacecraft
摘要
在航天器热平衡方程的基础上, 分析了表面涂层材料热辐射性质或布局调整对内热源变化和轨道变化的适应能力, 并对若干情形进行了定量分析。研究表明, 该方法有利于继承和保持成熟的航天器平台技术, 提高了对不同类型轨道的航天器热设计的灵活性。
Abstract
The adjustment of thermal radioactive property or distribution of surface coating materials could be applied to spacecraft thermal design. Their adaptive ability for variation of spacecraft internal heat source or orbit is analyzed based on the thermal equilibrium equation. These methods are beneficial to carry on previous platform technology, simultaneously, increase the flexibility of spacecraft thermal design.
刘必鎏, 王雯雯, 宋庆雷, 王永强, 席博. 基于航天器表面涂层材料的热设计分析及应用[J]. 红外技术, 2011, 33(5): 305. LIU Bi-liu, WANG Wen-wen, SONG Qing-lei, WANG Yong-qiang, XI Bo. Thermal Design Analysis and Application on the Surface Coating Materials of Spacecraft[J]. Infrared Technology, 2011, 33(5): 305.
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