首页> 外文会议>Conference on High-Power Laser Ablation IV Pt.2, Apr 22-26, 2002, Taos, NM, USA >Simulation of the plume generated by a micro laser-ablation plasma thruster
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Simulation of the plume generated by a micro laser-ablation plasma thruster

机译:微型激光烧蚀等离子推进器产生的羽流的仿真

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An end-to-end model is presented of the transient plume created by a micro laser-ablation plasma thruster. The laser ablation and plasma formation processes are modeled using a semi-analytical approach. This procedure provides boundary conditions at the target surface for the plume model that is based on a particle computational approach. The present study considers a 2 W diode-based laser irradiating a poly-vinyl chloride target over a spot radius of 10 μm for a pulse length of 100 μsec. The plume simulations reveal many details of the multi-component plasma expansion. The results are used to predict plume induced contamination effects.
机译:提出了由微型激光烧蚀等离子体推进器产生的瞬态羽流的端到端模型。使用半分析方法对激光烧蚀和等离子体形成过程进行建模。此过程基于粒子计算方法为羽状模型提供了目标表面的边界条件。本研究考虑了一个2 W二极管激光器,该激光器在10μm的光斑半径上照射聚氯乙烯靶,脉冲长度为100μsec。羽流模拟揭示了多组分等离子体膨胀的许多细节。该结果用于预测羽流引起的污染影响。

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