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载人航天器泄复压地面模拟试验方法
引用本文:张昊,魏传锋,李英斌,满广龙,赵丕盛.载人航天器泄复压地面模拟试验方法[J].航天器工程,2012,21(4):106-110.
作者姓名:张昊  魏传锋  李英斌  满广龙  赵丕盛
作者单位:1. 中国空间技术研究院,北京,100094
2. 航天医学工程研究所,北京,100094
摘    要:为获得泄复压时间曲线,验证载人航天器泄复压系统功能,须进行泄复压地面模拟试验。文章介绍了应用于载人航天器的泄复压试验方法,通过理论计算和试验结果对比,表明了试验方法的正确性和有效性,可为载人航天器后续型号整舱泄复压地面试验提供参考。

关 键 词:载人航天器  泄复压  地面模拟  试验方法

Simulation Test Method of Manned Spacecraft Depressurization and Repressurization
ZHANG Hao,WEI Chuanfeng,LI Yingbin,MAN Guanglong,ZHAO Pisheng.Simulation Test Method of Manned Spacecraft Depressurization and Repressurization[J].Spacecraft Engineering,2012,21(4):106-110.
Authors:ZHANG Hao  WEI Chuanfeng  LI Yingbin  MAN Guanglong  ZHAO Pisheng
Institution:1 China Academy of Space Technology,Beijing 100094,China)(2 Institute of Space Medico-engineering,Beijing 100094,China)
Abstract:To obtain the time curve of depressurization and repressurization for validating depressurization and repressurization system’s function,the simulation test of depressurization and repressurization is required to be operated.The test method based on manned spacecraft sealed cabin is introduced in this paper.The comparion between calculated result and test data demonstrates the correctness and validity of the method.This method can be used to design the depressurization and repressurization test of subsequent manned spacecraft.
Keywords:manned spacecraft  pressure releasing and recovering  simulation test  test method
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