等离子体鞘套的地面模拟、测量和主动干预

      Ground simulation, measurement and active intervention of reentry plasma sheath

      • 摘要: 高超音速航天飞行器再入空间大气层时,由于激波加热和热化学防护材料的烧蚀等原因,会在飞行器表面形成致密的等离子体鞘套。鞘套的形成会造成无线电通讯信号的中断,因此,减轻和消除黑障对遥测设备通讯和国防安全至关重要。想要减轻和消除黑障,首先需要了解黑障中的等离子体电子密度参数信息。为了解决这一问题,我们首先提出了一种新型复合探针,可以实时、有效的探测黑障高温流场中的电子密度参数信息;同时在地面模拟空间等离子体实验装置中完成复合探针的数据采集,比对和模型修正,所得结果与其它探测设备进行比对,不确定度小于17%;两种探针技术相互独立工作,又相辅相成,互相比对。其次开展亲电子物质释放试验,可以有效的降低流场等离子体中的电子密度参数信息,最终服务于国家航天航空部门等。本文将对该方面的研究工作进行一个系统性的综述。

         

        Abstract: When hypersonic spacecraft reenters the space atmosphere, the dense plasma sheath will be formed on the surface of hypersonic spacecraft due to shock wave heating and ablation of thermochemical protective materials. The formation of sheath will cause the interruption of radio communication signals so that the reduction and elimination of black barriers are essential for telemetry equipment communication and national defense security. It is necessary to know the information on plasma electron density parameters in the black barrier and then could reduce and eliminate the black barrier. In order to solve this problem, the first, a novel composite probe was proposed by us, which can diagnose the electron density parameters in the high-temperature flow field plasma in real-time and effectively. At the same time, the data acquisition, comparison and model modification of the composite probe were completed in the ground simulated space plasma experimental equipment. The results were compared with other detection equipment, and the uncertainty was less than 17%. The two probe techniques work independently of each other, and complement each other and compare with each other. Secondly, the release test of electrophilic substances can effectively reduce the electron density parameter information and finally serve the national aerospace department. This paper will make a systematic review of the research work in this field.

         

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