中国空间科学技术

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舱外航天服热试验方法研究

范含林;孙萌;李潭秋;吴志强;张堪;潘维;   

  1. 北京空间飞行器总体设计部;中国航天员科研训练中心;
  • 发布日期:2009-10-25

Research on Thermal Test Methods for Extravehicular Mobility Unit

Fan Hanlin1 Sun Meng1 Li Tanqiu2 Wu Zhiqiang2 Zhang Kan1 Pan Wei1(1 Beijing Institute of Spacecraft System Engineering,Beijing 100094)(2 Astronaut Center of China,Beijing 100094)   

  • Online:2009-10-25

被引次数

9

摘要： 舱外航天服采用主被动相结合的热控方式控制内部的温度,但其外形复杂,影响外热流的因素很多,因此舱外航天服热试验存在着与传统航天器热试验完全不同的特点。文章根据舱外航天服热设计的特点,对舱外航天服的地面热试验方法进行了比较分析和研究,论证了采用等效外热流模拟方法,通过进行舱外航天服系统漏热和散热能力的测试来验证热设计方法的合理性及热试验方法的可行性。

关键词: 舱外航天服, 散热能力, 热试验, 载人航天器

Abstract: Active thermal control technologies were used in extravehicular mobility unit(EMU).The configuration of EMU is complicated and there are many influence factors on reaching heat flux.The thermal test for EMU had the different characters with that of traditional space probe.Different simulation methods of EMU thermal test were presented,based on the characteristics of the thermal design.It′s feasible to validate the thermal design by equivalently simulating the space heat flux as the test thermal boundary and measuring the heat leakage of the EMU and heat dissipation ability.