Micro-satellites thermal control - concepts and components
Micro-satellites thermal control - concepts and components
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DOI：
10.1016/j.actaastro.2004.09.003
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发表时间：
2005-01-01
影响因子：
3.5
通讯作者：
Baturkin, V
中科院分区：
文献类型：
--
作者：
Baturkin, V
本文的主要思想是目前的趋势，在微型卫星热控制概念，可以是合理的和有用的后续任务，由于这种类型的卫星的密集扩展的调查。为了这个目的。利用了乌克兰国立技术大学在为微型卫星Magion 4号、5号、BIRD和行星间飞行任务VEGA、PHOBOS自主热控制系统设计热控制硬件过程中获得的参考资料和经验教训。分析时考虑的主要参数是卫星的大小。马萨诸塞州功率消耗、轨道参数、高度控制特性和热控制描述。被动热控制概念被广泛应用，除了对敏感部件的自主温度调节：例如电池，高精度光学器件和某些类型的传感器。多层隔热、光学镀膜、导热元件等实现被动热控制设计的实用手段。简要描述了垫圈。(C)2004 Elsevier Ltd.保留所有权利。
The main idea of this paper is to present the survey of current tendencies in micro-satellites thermal control concepts that can be rational and useful for posterior missions due to intensive expansion of satellites of such type. For this purpose. the available references and lessons learned by the National Technical University of Ukraine during the elaboration of thermal control hardware for micro-satellites Magion 4, 5, BIRD and autonomous thermal control systems for interplanetary missions VEGA, PHOBOS have been used. The main parameters taken into consideration for analysis are the satellite sizes. mass. power consumption, orbit parameters, altitude control peculiarities and thermal control description. It was defined that passive thermal control concepts are widely used, excepting autonomous temperature regulation for sensitive component: such as batteries, high-precision optics, and some types of sensors. The practical means for realization of passive thermal control design as multi-layer insulation, optical coatings, heat conductive elements. gaskets are briefly described. (C) 2004 Elsevier Ltd. All rights reserved.