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离子发动机加速栅极腐蚀深度的DFF测量与数值模拟
引用本文:刘畅,汤海滨,张振鹏,姜志国,顾左,李娟.离子发动机加速栅极腐蚀深度的DFF测量与数值模拟[J].航空动力学报,2008,23(3):574-579.
作者姓名:刘畅  汤海滨  张振鹏  姜志国  顾左  李娟
作者单位:1. 北京航空航天大学,宇航学院,北京,100083
2. 兰州物理研究所,兰州,730000
基金项目:国家自然科学基金(50306001)
摘    要:使用聚焦深度表面测量(DFF)方法对加速栅极下游表面腐蚀深度进行了测量,并将测量结果与数值模拟结果进行了比较,所使用的数值方法为PIC-Monte Carlo方法.利用数值模拟程序对离子发动机栅极腐蚀进行了数值模拟.以氙为推进剂,栅极材料为钼.用蒙特卡罗方法模拟了氙离子与中性氙原子之间的电荷交换碰撞.模拟得到了加速栅极下游表面离子溅射腐蚀的深度分布,腐蚀模式与"Pits and grooves"模式相吻合.

关 键 词:航空、航天推进系统  栅极  腐蚀  溅射  聚焦深度表面测量
文章编号:1000-8055(2008)03-0574-06
收稿时间:2007/3/19 0:00:00
修稿时间:2007年3月19日

Numerical simulation and DFF measurement of ion thruster accelerator grid erosion depth
LIU Chang,TANG Hai-bin,ZHANG Zhen-peng,JIANG Zhi-guo,GU Zuo and LI Juan.Numerical simulation and DFF measurement of ion thruster accelerator grid erosion depth[J].Journal of Aerospace Power,2008,23(3):574-579.
Authors:LIU Chang  TANG Hai-bin  ZHANG Zhen-peng  JIANG Zhi-guo  GU Zuo and LI Juan
Institution:School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China;School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China;School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China;School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China;Lanzhou Institute of Physics, Lanzhou, 730000, China;Lanzhou Institute of Physics, Lanzhou, 730000, China
Abstract:Particle simulation of ion thruster grids was carried out via particle-in-cell(PIC) method and numerical method for calculating the erosion depth of the accelerator grid downstream surface was developed.Xenon was used as propellant and Molybdenum was used as grid material.Monte Carlo method was adopted to simulate the charge exchange collisions between Xenon ions and atoms.Distribution of erosion depth of the downstream surface of accelerator grid was obtained,and the erosion pattern agreed with the "pits and grooves" erosion pattern.Depth from focus(DFF)method was used to measure the erosion depth of the downstream surface of the accelerator grid and comparison between the measured and calculated erosion depth was carried out.
Keywords:aerospace propulsion system  grids  erosion  sputtering  depth from focus(DFF)
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