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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:数值模拟的探空火箭电离层等离子体:影响ofmagnetic字段后形成和火箭的潜力

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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:的充电在亚音速和探空火箭超音速等离子体与外部磁流与数值particle-in-cell领域研究(图片)模拟。政权被认为是相对应的电离层₂层,电子强磁化,磁化离子是虚弱的。磁场取向的影响浮动的火箭和潜力增加火箭轴之间的角度磁场方向火箭的潜力变得不那么消极。产生不对称后的下游火箭发射的。密度可以延长30电子德拜长度;这些等离子体扰动分析原位测量。仿真结果和实际测量探空火箭也显示。

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