多粒度火箭喷焰尘埃等离子体云空间扩散效应研究
首发时间:2015-12-10
摘要:火箭喷焰尘埃等离子体云是人类活动对大自然造成干扰的一个特殊现象,会明显影响电离层特性。对多粒度火箭喷焰尘埃等离子体云,采用单粒子轨道模型的粒子仿真方法,模拟了不同粒径带电尘埃粒子在电离层中的扩散过程,分析粒径对尘埃等离子体云时空演变过程的影响。研究结果表明:多粒度分布的火箭喷焰尘埃等离子体云最终扩散结果是形成一个不同高度、不同区域和不同大小的多个云团混杂的不均匀空间结构;小粒径尘埃粒子受地磁场作用明显,会发生长距离水平漂移,直径1nm的尘埃粒子约向东漂移80km,并最终形成悬停位置相对较高,面积相对较小的云团;大粒径尘埃粒子受地磁场作用较弱,直径100nm的尘埃粒子基本不发生东西漂移,最终形成悬停位置相对较低,面积较大的云团;粒子在洛仑兹力作用下的水平漂移和重力及压力梯度下的垂直下降均呈先加速后逐渐减小到0的演化规律;对于垂直下降运动,粒径较大的粒子其加速和减速过程都相对较快,可迅速到达悬停高度,而粒径较小的粒子加速和减速过程相对较慢,到达悬停高度的时间也相对较长。
关键词: 航空宇航推进理论与工程 尘埃等离子体 粒子模拟 扩散
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Study on the diffusion of rocket plume dusty plasma cloud with multi particle size
Abstract:Rocket plume dusty plasma cloud is a special phenomenon in human activities, which causes interference to the nature, and significantly affects the ionosphere characteristics. The diffusion process of different diameter particle in the rocket plume dusty plasma cloud was simulated with single particle trajectory -- a particle simulation method, and the influence of particle size on the diffusion was analyzed. The research results show that: the rocket plume plasma dust cloud with multi particle size distribution eventually spread results in the formation of uneven spatial structure of a different height, different regions and different sizes of a plurality of mixed clouds; the earth's magnetic field effect is more obvious on small particle, which will drive the eastward drift; the drift distance of particle with 1nm diameter is about 80km, with a relatively higher hovering position and smaller area; while almost no drift and a relatively lower hovering position and bigger area for the dust particle with 100nm diameter; the vertical downward under the gravity and pressure gradient, as well as the horizontal drift with the Lorentz force show a gradual slowdown after the acceleration; for vertical downward motion, the acceleration and deceleration process of larger size particle is relatively faster, which arrives in the hovering position rapidly, while the small particle is slower and the time arriving in the hovering position is relatively longer.
Keywords: Aerospace propulsion theory and engineering;dusty plasma particle simulation diffusion
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