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Design and On-orbit Performance Evaluation of Thermal Control System for SHENZHOU-7 Spaceship

Huang Jiarong Fan Yufeng Liu Bingqing Lu Wei(Beijing Institute of Spacecraft System Engineering,Beijing 100094)   

  • Online:2009-10-25

Abstract: The on-orbit flight data were analyzed and the operation performance was evaluated.Flight test shows that TCS has excellent temperature adjust and adapt abilities during prelaunch and ascent stages,orbit flight,EVA and reentry phases,and all apparatus temperature,air temperature and air relative humidity meet the technology requirements.