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Use of a helicon source for development of a re-entry blackout amelioration system.

机译:使用螺线管源开发再入停电改善系统。

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摘要

During atmospheric re-entry and hypersonic flight, a bow shock forms around the vehicle leading edge. The air becomes super-heated as it passes through the shock, ionizes and forms a plasma sheath. This sheath prevents transmission of electromagnetic waves with frequencies similar to those used for radio communications. This phenomenon is referred to as the "communications blackout." In this dissertation, hypersonic communications blackout is studied, and a method for ameliorating the blackout is presented.;A plasma source was designed and built for the purpose of simulating a re-entry plasma sheath. The plasma number density in a re-entry plasma sheath ranges from 1014 m--3 to 1018 m--3. A helicon source was chosen to simulate the conditions during atmospheric re-entry because it produces high-density plasma while maintaining that density downstream of the source. For this reason, and because the electron temperature downstream of the source (1 eV to 6.5 eV) is of a similar order of magnitude as that found during re-entry (0.4 eV to 1 eV), the helicon source was deemed appropriate. The Plasmadynamics and Electric Propulsion Laboratory helicon source was found to produce an upstream ion number density of 2.5 x 1019 m--3. Downstream, where experiments with the plasma amelioration system were performed, the number density ranged from 0.55 x 1017 m--3 to 3.3 x 1017 m--3, which represent altitudes between 65 km and 75 km.;After characterizing the helicon plasma source, the amelioration system was placed downstream. The re-entry and hypersonic vehicle plasma communications (ReComm) system consists of a single solenoid electromagnet with two electrodes perpendicular to the magnetic field. The crossed fields direct plasma away from a region surrounding an antenna, creating a "window" in the sheath through which radio signals can pass. Langmuir probe, hairpin resonance probe and signal attenuation measurements show that the system is effective at reducing the number density to 80% of that measured when no fields are present. However, the system did not perform as expected. The majority of the reduction occurred with only the presence of the magnetic field. Possible explanations were studied using both analytical methods and COMSOL to model the fields. The shape of the magnetic field itself contributed greatly to the plasma number density reduction.
机译:在大气再进入和高超音速飞行期间,在飞行器前缘周围形成弓形冲击。空气在通过冲击时变得过热,离子化并形成等离子体鞘。该护套可防止电磁波以类似于无线电通信的频率传输。这种现象称为“通信中断”。本文对高超声速通信停电进行了研究,提出了一种改善停电的方法。设计并建立了等离子体源,用于模拟再入等离子体鞘。再入等离子体鞘层中的等离子体数密度范围为1014 m--3至1018 m--3。选择螺线管源来模拟大气再入期间的条件,因为它会产生高密度等离子体,同时保持该源下游的密度。出于这个原因,并且由于源下游的电子温度(1 eV至6.5 eV)与重新进入过程中发现的电子温度(0.4 eV至1 eV)具有相似的数量级,因此认为螺线管源是合适的。发现等离子体动力学和电力推进实验室的螺旋源产生的上游离子数密度为2.5 x 1019 m--3。下游,进行了等离子体改善系统的实验,其数密度范围为0.55 x 1017 m--3至3.3 x 1017 m--3,代表65 km至75 km之间的高度。 ,改善系统放置在下游。再入和超音速车辆等离子体通信(ReComm)系统由一个电磁线圈电磁体组成,该电磁体具有两个垂直于磁场的电极。交叉的场使等离子体远离天线周围的区域,从而在护套中形成一个“窗口”,无线电信号可以通过该窗口。 Langmuir探针,发夹共振探针和信号衰减测量结果表明,该系统可有效地将数字密度降低到不存在电场时所测数字密度的80%。但是,系统没有按预期运行。减少的大部分仅在磁场的存在下发生。使用分析方法和COMSOL对字段进行建模,研究了可能的解释。磁场的形状本身对等离子体数目密度的降低有很大的贡献。

著录项

  • 作者

    Lemmer, Kristina Marian.;

  • 作者单位

    University of Michigan.;

  • 授予单位 University of Michigan.;
  • 学科 Engineering Aerospace.
  • 学位 Ph.D.
  • 年度 2009
  • 页码 213 p.
  • 总页数 213
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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