Hall推力器羽流数值模拟

推进技术 ›› 2008, Vol. 29 ›› Issue (1): 93-97.

Hall推力器羽流数值模拟

钱中,王平阳,杜朝辉,康小录

上海交通大学航空航天工程系上海200240;上海交通大学航空航天工程系上海200241;上海交通大学航空航天工程系上海200242;上海航天动力机械研究所上海200233

发布日期:2021-08-15
基金资助:
国家自然科学基金资助项目(50306013)

Numerical simulation of hall thruster plume

Dept.of Aerospace Engineering,Shanghai Jiaotong Univ,Shanghai 200240,China;Dept.of Aerospace Engineering,Shanghai Jiaotong Univ,Shanghai 200241,China;Dept.of Aerospace Engineering,Shanghai Jiaotong Univ,Shanghai 200242,China;Shanghai Spaceflight Inst.of Power Machinery,Shanghai 200233,China

Published:2021-08-15

摘要/Abstract

摘要： 以稳态等离子体推力器(SPT)羽流流场为研究对象,基于直接蒙特卡罗模拟与粒子单元混合方法建立数值模型,模拟等离子体稳态流动,研究流场特性。将计算结果与实验数据相比较,并与同类推力器羽流参数进行比较,以保证仿真可靠性。研究表明,所建立的仿真模型能够较好地预测SPT羽流电子数密度和离子电流密度等参数。

关键词: 稳态等离子推力器;羽流;蒙特卡罗法;粒子单元法;数值仿真

Abstract: A numerical model,based on the direct simulation Monte Carlo and particle-in-cell hybrid method,was developed to simulate the steady flow of plasma and study the characteristics of the plume.The computational results were compared with both experimental data and plume parameters of a congener thruster to ensure the reliability of simulation.It indicated that the simulation model was able to well predict both electron number density and ion current density of plume of SPT.

Key words: Stationary plasma thruster;Plume;Direct simulation Monte Carlo;Particle-in-cell hybrid method;Numerical simulation

钱中,王平阳,杜朝辉,康小录. Hall推力器羽流数值模拟[J]. 推进技术, 2008, 29(1): 93-97.