Abstract:
To study the evacuation process of the working fluid for in-orbit spacecraft, a lunar gravity experimental system is built and the influence factors on the evacuation speed of the working medium are studied. The variation of the pressure and the temperature inside the pipelines are obtained in the process of the fluid evacuation. It is indicated that the pipeline temperature remains basically unchanged in the whole emission process, and that the initial pressure, the local temperatures and the outlet temperature all have little effect on the evacuation rate.