低空环境中多层隔热组件的破坏机理研究及防护

The failure mechanism of multilayer insulation (MLI) in low-altitude environment and its protection

  • 摘要: 不同于国内外航天器110 km以上高度的常规抛罩,设定卫星在67 km低空环境下抛罩,针对此情况下主动段气流对星外多层隔热组件的破坏机理进行研究。多层隔热组件的破坏是剪切力和材料鼓胀力的综合作用。通过理论分析和风洞冲刷试验,确定了星外多层隔热组件的防护方案,并且已经经过在轨飞行试验的验证。

     

    Abstract: The protective fairings designed to bear the brunt of heating are generally jettisoned at an altitude of above 110 km. However, a satellite may work at an altitude of below 67 km. This paper studies the specific conditions in the low-altitude environment, focusing on the failure mechanism of multilayer insulation (MLI) affected by ascent airflow. The results show that the failure of MLI is due to the combined action of shearing force and material’s expansive force. A shielding scheme for MLI is put forward based on the analysis and is validated by the experiment in wind tunnel. The shielding measurement for MLI is confirmed by the real flights.

     

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