中国空间科学技术

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卫星密封舱湿度控制技术的应用研究

张加迅;李劲东;孙耀赤;   

  1. 中国空间技术研究院,中国空间技术研究院,兰州物理研究所 北京100094,北京100094,730000
  • 发布日期:2006-06-25

Application Study on Humidity Control Technique for the Pressurized Module in Satellites

Zhang Jiaxun Li Jindong(China Academy of Space Technology,Beijing 100094)Sun Yaochi(Lanzhou Physics Research Institute,Lanzhou 730000)   

  • Online:2006-06-25

被引次数

8

摘要： 通过实验验证和热力学分析相结合的方法,对卫星密封舱湿度控制技术进行了应用研究。由卫星的热试验和在轨飞行试验可知,通过利用相机胶片的水汽含量、设置湿控子系统及进行临射前舱内湿度调控等方法,能够使卫星密封舱内局部区域的相对湿度控制在30%~60%的范围内,满足相机要求。通过研究可得,热控系统所采取的卫星湿度控制技术是成功的,保证了卫星任务的圆满完成。

关键词: 湿度控制, 热控制, 密封舱, 人造卫星, 应用, 研究

Abstract: In order to solve the humidity requirements of the camera in the satellite,the(application) study on the humidity control technique for the pressurized module is conducted by(experimental) verification and thermodynamic analysis.By the thermal test and in-orbit test of the satellite,it can be got that,by using the moisture of the camera's film,using humidity control(subsystem) and conducting humidity adjustment before launch,the relative humidity of the local area in the pressurized module of the satellite can be controlled in a range about 30%~60%,which meets the requirements of the camera.It is concluded from the paper that,the humidity control technique used by the thermal control system is successful,and ensure the full success of the(satellite's) task.