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Plasma wave radiation induced by a conducting tethered satellite system.

机译:传导性束缚卫星系统引起的等离子波辐射。

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摘要

During the planned electrodynamic tethered satellite system (TSS-1) experiment, a large, conducting subsatellite will be tethered to the space shuttle. The long, surface-insulated tether wire will electrically couple the two satellites, thereby forming a large conductor which moves in a magnetized plasma. One of the scientific objectives of the experiment will be the excitation of plasma waves.;It is shown that the model current system radiates in two discrete frequency bands. Band I (0 ;A new model is constructed here which shows the relationship between the various wavelengths in the plasma and the moving current source. In particular, it is shown that the low frequency waves form a large, co-moving structure in which oppositely charged wave surfaces in the plasma are matched to the two ends of the tethered system. At these frequencies the system is a single, large, coherent radiation source. In the high frequency band, however, the waves are produced locally by the motion and charge interaction of the satellite's conducting surface. Here, the two ends of the system are completely independent, localized, radiation sources. The conclusion of the theoretical model is that the total radiated power is maximized by (1) reducing the diameter of the satellite, (2) eliminating plasma sheath formation, and (3) drawing the highest possible current to the satellite's outer surface.;This thesis considers the processes of wave excitation through theoretical models and constructs estimates of the total radiated power and frequency spectrum. It is shown that wave excitation arises not directly from the current flow within the tethered system but rather the collection of this current from the plasma at the two uninsulated ends. The wave radiation is thus found to be critically dependent on the current distribution at the tethered system's end-connectors. A new current system is therefore developed which models current collection by a large, spherical satellite.
机译:在计划进行的电动系留卫星系统(TSS-1)实验期间,将把一个大型的导电亚卫星拴系在航天飞机上。表面绝缘的长束线将两个卫星电耦合,从而形成一个较大的导体,该导体在磁化的等离子体中移动。实验的科学目的之一是激发等离子体波。证明模型电流系统在两个离散频带中辐射。 Band I(0;这里构造了一个新模型,该模型显示了等离子体中各种波长与移动电流源之间的关系。特别是,它表明低频波形成了一个大的共同移动的结构,其中相反等离子体中的带电波表面与系留系统的两端相匹配,在这些频率下,系统是一个单一的,大的,相干的辐射源,但是在高频带中,这些波是由运动和电荷局部产生的卫星传导表面的相互作用。在这里,系统的两端是完全独立的,局部的辐射源。理论模型的结论是,通过(1)减小卫星的直径,总辐射功率最大。 2)消除等离子体鞘的形成,以及(3)向卫星的外表面吸收尽可能大的电流。构造总辐射功率和频谱的估计值。结果表明,波激发不是直接由系留系统中的电流引起的,而是由在两个未绝缘的末端从等离子体中收集的电流引起的。因此,发现波辐射严格取决于系留系统末端连接器上的电流分布。因此,开发了一种新的电流系统,该系统可以对大型球形卫星的电流收集进行建模。

著录项

  • 作者

    Donohue, Denis Joseph.;

  • 作者单位

    Stanford University.;

  • 授予单位 Stanford University.;
  • 学科 Plasma physics.;Aerospace engineering.
  • 学位 Ph.D.
  • 年度 1991
  • 页码 221 p.
  • 总页数 221
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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