摘要
微纳卫星的发展需要新型高效热控技术,基于石墨烯的高效热控系统实施于微纳卫星主结构上,对降低热点温度,拉均星内温度有良好效果。论文介绍了基于石墨烯的微纳卫星热控结构组成及特性,及对这一热控结构在真空高低温下传热特性的测试系统搭建及试验研究。
The development of micro-nano satellites requires a new type of high-efficiency thermal control technology. The high-efficiency thermal control system based on graphene is implemented on the main structure of micro-nano satellites,which has good effect on reducing hot spot temperature and balancing average temperature inside satellites. In this paper,the composition and characteristics of graphene-based thermal control structures of micro-nano satellites are introduced,and the testing system of heat transfer characteristics of this thermal control structure under vacuum and high and low temperature is built and tested.
出处
《机电产品开发与创新》
2017年第5期4-6,共3页
Development & Innovation of Machinery & Electrical Products
关键词
高效热控
真空高低温
传热特性测试
high-efficiency thermal control
vacuum and high and low temperature
test on heat transfer characteristics