Chinese Space Science and Technology

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Vacuum Thermal Test Technology for Large Spacecraft

Pang Hewei Huang Bencheng Qian Beixing Jia Yang (Beijing Institute of Spacecraft Environment Engineering, Beijing 100029)   

  • Online:2002-06-25

Abstract: The vacuum thermal test technologies for large spacecraft in KM6 space environment simulator, including thermal balance test technology and thermal vacuum test technology, are introduced in this paper. Test objectives, test description, test phases, flux control and support hardware are introduced too.