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舱外航天服的轨道空间外热流计算方法
引用本文:邱义芬,陈拥华,袁修干,杨春信.舱外航天服的轨道空间外热流计算方法[J].航空学报,2004,25(3):221-224.
作者姓名:邱义芬  陈拥华  袁修干  杨春信
作者单位:北京航空航天大学,航空科学与工程学院,北京,100083
基金项目:国家863计划(2002AA743033)资助项目
摘    要: 分析了舱外航天服在轨道空间环境的辐射换热热流。采用蒙特卡罗(MonteCarlo)法,计算了航天服及飞船处于各种相对位置时,航天服对飞船的红外辐射角系数;航天服相对于地球位于各种位置时,航天服对地球的红外辐射角系数;在一定太阳照射方向下,飞船及地球对航天服的太阳反射角系数。与文献数据比较,证明此方法计算舱外航天服空间外热流适用性强,结果准确、可靠,能满足工程使用要求。

关 键 词:热控制  空间外热流  蒙特卡罗法  航天服  辐射角系数  
文章编号:1000-6893(2004)03-0221-04
修稿时间:2003年4月21日

A Method of Calculating External Heat Flux on Spacesuit Used for EVA
QIU Yi-fen,CHEN Yong-hua,YUAN Xiu-gan,YANG Chun-xin.A Method of Calculating External Heat Flux on Spacesuit Used for EVA[J].Acta Aeronautica et Astronautica Sinica,2004,25(3):221-224.
Authors:QIU Yi-fen  CHEN Yong-hua  YUAN Xiu-gan  YANG Chun-xin
Institution:School of Aeronautics Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
Abstract:The orbital radiation heat flux received by the spacesuit used for extravehicular activity ( EVA )is analyzed. By Monte Carlo method, the reflection and infrared radiation angle factors are calculated between spacesuit and spacecraft or earth when spacesuit is located at any position relative to the spacecraft or the earth. It shows that the method is applicable and the results obtained are accurate and reliable as compared with data of References, so as to entirely meet the requirement of engineering application.
Keywords:thermal control  orbital heat flux  Monte Carlo method  spacesuit  radiation angle factor
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