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Observation of plasma waves around the wake of an ionospheric sounding rocket

机译:观察电离层探测火箭尾围绕的等离子体波

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When a body moves in plasma at a supersonic velocity, a rarefied plasma region called ‘plasma wake’ is formed behind the body. A wake is formed behind a body which is immersed in a plasma flow such as an artificial satellite and an ionospheric sounding rocket as well as a solar system body immersed in solar-wind plasma. Although there are several studies which report plasma waves around the wakes of a satellite [1] and of the moon [2], little attention has been given to plasma waves in association with the rocket wake. However, observational results from two rocket experiments performed in 1998 [3] and 2012 have suggested the generation of plasma waves around the wake of a rocket. It is very important to reveal the generation process of plasma waves near the rocket wake for understanding the universal physics related to the interaction between streaming plasma and a non-magnetized body as well as for interpreting wave data obtained in rocket experiments more accurately. In the S-520-26 rocket experiment in 2012, with an impedance probe and a wave receiver, we measured the electron number density and plasma waves at 260-msec interval, which corresponds to one-fourth or one-fifth of the spin period of the rocket. During the flight, three kinds of plasma waves were observed. Based on the presumption that the observed waves are caused just near the wake of the rocket, they must be short-wavelength electrostatic waves such as electrostatic electron cyclotron harmonic (ESCH) waves, upper hybrid resonance (UHR) mode waves, and whistler mode waves. In order to discuss the generation mechanisms of the waves, we calculate linear growth rates of electrostatic waves with assumptions of an anisotropic electron distribution function which has a beam component or temperature anisotropy. Consequently, we obtain positive growth rates in frequency ranges similar with some of the observed waves. We also reveal the spatial distribution of the wave activities around the- rocket and its relationship with the wake structure by analyzing the spin-phase dependence of the waves and the electron number density we observed. The spin-phase dependence suggests that there are localized hot plasmas around the wake structure, which can stimulate plasma instabilities. In this presentation, we clarify the frequency range and spatial distribution of the plasma waves around the wake based on the analyses of the data from the S-520-26 rocket experiment. We also discuss the velocity distribution of electrons which can drive instabilities generating the plasma waves as we observed.
机译:当主体在超声速度下以等离子体移动时,在主体后面形成称为“等离子体唤醒”的稀土等离子体区域。在浸入诸如人造卫星和电离层探测火箭的等离子体流的体内形成尾巴,以及浸入太阳能血浆中的太阳能系统体。虽然有几项研究报告卫星[1]和月亮醒来的等离子体波[2],但是已经对与火箭唤醒结合的等离子体波很少注意。然而,1998年进行的两个火箭实验的观察结果[3]和2012建议在火箭尾部围绕着围绕火箭的产生等离子体波。揭示火箭唤醒附近的等离子体波的生成过程非常重要,以了解与流等离子体和非磁化机体之间的相互作用相关的通用物理以及更准确地将火箭实验中获得的波数据解释。在2012年的S-520-26火箭实验中,通过阻抗探头和波浪接收器,我们以260-毫秒间隔测量电子数密度和等离子体波,其对应于旋转时段的四分之一或五分之一火箭。在飞行期间,观察到三种等离子体波。基于所观察到的波在火箭尾部引起的推测,它们必须是诸如静电电子回旋谐波(ESCH)波的短波长静电波,上混合谐振(UHR)模式波和吹口机模式波。为了讨论波的生成机制,我们计算静电波的线性生长速率,具有具有梁部件或温度各向异性的各向异性电子分布函数的假设。因此,我们获得与一些观察波类似的频率范围的正增长率。我们还通过分析波浪的自旋相位依赖性和我们观察到的电子数密度,揭示了火箭周围的波浪活动的空间分布及其与唤醒结构的关系。旋转相位依赖表明,唤醒结构周围有局部的热等离子体,这可以刺激等离子体稳定性。在本演示文献中,根据来自S-520-26火箭实验的数据的分析,我们阐明了唤醒周围的等离子体波的频率范围和空间分布。我们还讨论了当我们观察到时,可以驱动稳定性的电子的速度分布。

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