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Numerical simulations of a sounding rocket in ionospheric plasma: Effects ofmagnetic field on the wake formation and rocket potential

机译:电离层等离子体探测火箭的数值模拟:磁场对唤醒形成和火箭电位的影响

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摘要

The charging of a sounding rocket in subsonic and supersonic plasma flows with external magnetic field is studied with numerical particle-in-cell (PIC) simulations. A weakly magnetized plasma regime is considered that corresponds to the ionospheric F_2 layer, with electrons being strongly magnetized, while the magnetization of ions is weak. It is demonstrated that the magnetic field orientation influences the floating potential of the rocket and that with increasing angle between the rocket axis and the magnetic field direction the rocket potential becomes less negative. External magnetic field gives rise to asymmetric wake downstream of the rocket. The simulated wake in the potential and density may extend as far as 30 electron Debye lengths; thus, it is important to account for these plasma perturbations when analyzing in situ measurements. A qualitative agreement between simulation results and the actual measurements with a sounding rocket is also shown.
机译:利用数值粒子粒细胞(PIC)模拟,研究了具有外部磁场的亚音速和超音速等离子体流动中的发声火箭的充电。 考虑弱磁化的等离子体状态,其对应于电离层F_2层,电子被强磁化,而离子的磁化是弱的。 据证明磁场取向影响火箭的浮动电位,并且在火箭轴和磁场方向之间的角度增加到火箭电位变得更少。 外部磁场引起火箭下游的不对称唤醒。 潜在和密度的模拟唤醒可以延伸到30个电子德义长度; 因此,重要的是在分析原位测量时考虑这些血浆扰动。 还示出了仿真结果与具有探测火箭的实际测量之间的定性协议。

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