首页|离子推力器工作全过程数值仿真方案研究

离子推力器工作全过程数值仿真方案研究

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离子推力器具有比冲高、寿命长、推力连续可调等优点,已成为未来空间探测任务推进系统的首选.离子推力器产品的优化设计通常采用实验测量的手段来实现,现有的仿真软件均是针对离子推力器的各个组成组件来开发,忽略了组件之间的相互耦合,为此,亟待开发一款综合考虑各组成部件相互作用的离子推力器工作全过程数值仿真软件.离子推力器结构复杂,且涉及等离子体场、流场、电场、粒子间碰撞以及粒子与壁面相互作用等过程,现有的仿真手段很难实现在同一时空下的数值模拟.提出了一种近似耦合的数值仿真方法,即仍将离子推力器的各组成部件作为一个独立的个体来仿真,但在数值建模时,考虑相关联部组件的影响.分别构建了两两耦合的数值仿真模型,开展了数值仿真计算,仿真结果显示部组件单独工作和耦合工作时组件内部的等离子体微观参数将发生较大变化.
Investigation on the Numerical Design of the Beam Current Production Process of Ion Thruster
Ion thruster has become the first choice of the propulsion system for the future space exploration missions for its high specific impulse,long lifetime and continuous thrust adjustment.Optimization of the ion thruster is us-ually realized by large numbers of experimental tests.Current simulation models developed only focus on the components themselves and ignore the interactions between components.The professionally numerical model that takes these interactions relationship into account should be developed.However,the complicated structures and coupled interactions between plasma,electric potential,magnetic field,particle collisions,particles and walls,it isimpossible to simulate the working processes si-multaneously.A similar coupling simulation method is proposed,where the component itself is treated as a whole but it is simulated by giving the coupling interaction as the boundary conditions.Coupling simulation models of two components are established independently and their interactions are simulated.The results show that the plasma micro-parameter changes tremendously when it works alone or not.

ion thrusterworking processsimulation

陈娟娟、王江伟、郭宁、耿海、贾艳辉、徐金灵

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兰州空间技术物理研究所 真空技术与物理重点实验室,兰州 730000

中国空间技术研究院杭州中心,杭州 310000

离子推力器 工作全过程 数值仿真

国家自然科学基金真空技术与物理重点实验室基金甘肃省自然科学基金甘肃省自然科学基金

62371213614220721030322JR5RA78422JR5RA787

2024

真空与低温
中国航天科技集团公司第五研究院510研究所

真空与低温

CSTPCD
影响因子:0.567
ISSN:1006-7086
年,卷(期):2024.30(6)