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中型空间环境模拟器真空系统的设计与模拟

王娟;庄达民;王浚;   

  1. 北京航空航天大学,北京航空航天大学,北京航空航天大学 北京100083,北京100083,北京100083
  • 发布日期:2007-10-25

Design and Simulation of Medium Scale Space Environment Simulator Vacuum System

Wang Juan Zhuang Damin Wang Jun(Beijing University of Aeronauics and Astronautics,Beijing 100083)   

  • Online:2007-10-25
  • Supported by:
    国防基础科研项目(A2120060022)

摘要: 探讨了用于舱外航天服性能实验的中型空间环境模拟器真空系统的设计和模拟。通过对低温泵的真空度及其抽速与液氦低温板温度的关系进行模拟,验证了真空系统设计的合理性。对中型环境模拟系统预冷采用开放式液氮以简化系统结构;对系统的主要部件液氦低温板和辐射挡板进行了构造分析和热负荷计算;分析了液氦低温板的凝结层对低温泵性能的影响。通过对液氦低温板温度场进行模拟及分析,对液氦低温冷凝面进行了优化设计与性能验证。通过对航天员氧消耗量的分析合理估算了航天员自身代谢产热,据此确定了中型空间环境模拟系统热负荷及液氦供应量。

关键词: 热载荷, 低温泵, 液氦低温板, 真空系统, 中型空间环境仿真器, 航天服

Abstract: The design and simulation of the medium scale space environment simulator for the extravehicular activity space suit experiment were discussed.By simulating the temperature of the cryopanel and the relation between the pressure and pumping gas speed of the cryopump,it was verified the vacuum system design was rational.The pre-cooling of the medium scale space environment simulator adopted the open liquid nitrogen system in order to simplify system structure.The structure analysis and the radiation heat load computation were carried out from the cryopanel to the radiation baffle.The effects of the condensing layer of the cryopanel on the cryopump capabilities were analyzed.By simulating cryopanel temperature field and analyzing the maximum of temperature,the cryopanel design was optimized and the capabilities were verified.The oxygen wastage of the astronaut was analyzed to estimate the metabolism producing heat of the astronaut.The medium scale space environment simulator heat loads and the liquid helium demand of the cryopump were obtained.The system design and simulation of the medium scale space environment simulator provides the reference for the research of domestic astronaut extravehicular activity and correlative devices.