论文标题

迈向基于物理的超速粉尘影响模型

Toward a Physics Based Model of Hypervelocity Dust Impacts

论文作者

Kellogg, Paul J, Bale, S. D., Goetz, Keith, Monson, Steven J.

论文摘要

人们对高超音速粉尘影响在航天器传感器上产生电信号的过程有重要了解,从而使对物理学有更深入的了解。 Zaslavsky(2015)表明,最重要的信号来自航天器的充电,较少来自天线的充电。目前的工作是Zaslavsky的作品的延伸。提出了对超音速粉尘撞击物理学的分析处理,以及在传感器(天线)中产生电信号的机制。将治疗与立体声和帕克太阳能探针的观察结果进行了比较。通过模拟对这一过程的完整处理似乎超出了当前的计算机功能,但是治疗的某些部分必须取决于模拟,但可以通过分析治疗更好地理解其他功能。提出了与先前出版物相比,信号天线部分的贡献更大的证据。强调了静电力在形成退出的等离子云中的重要性。静电力导致逃逸云的迅速扩展,因此它比逃逸的膨胀速度更快,并且经常围绕一个或多个天线。这说明了偶极天线检测灰尘影响的能力。提出了一些直接充电的直接证据,以理解天线的偶尔负充电的一些进展。在没有进一步校准工作的情况下,将充电的实验室测量用于估计航天器撞击的大小是不可靠的。

There has been important understanding of the process by which a hypersonic dust impact makes an electrical signal on a spacecraft sensor, leading to a fuller understanding of the physics. Zaslavsky (2015) showed that the most important signal comes from the charging of the spacecraft, less from charging of an antenna. The present work is an extension of the work of Zaslavsky. An analytical treatment of the physics of a hypersonic dust impact and the mechanism for generating an electrical signal in a sensor, an antenna, is presented. The treatment is compared with observations from STEREO and Parker Solar Probe. A full treatment of this process by simulations seems beyond present computer capabilities, but some parts of the treatment can must depend on simulations but other features can be better understood through analytical treatment. Evidence for a somewhat larger contribution from the antenna part of the signal than in previous publications is presented. Importance of electrostatic forces in forming the exiting plasma cloud is emphasized. Electrostatic forces lead to a rapid expansion of the escaping cloud, so that it expands more rapidly than escapes, and frequently surrounds one or more antennas. This accounts for the ability of dipole antennas to detect dust impacts. Some progress toward an understanding occasional negative charging of an antenna is presented, together with direct evidence of such charging. Use of laboratory measurements of charge to estimate size of spacecraft impacts are shown to be not reliable without further calibration work.

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