Design optimization of a magnetoplasmadynamic thruster by numerical methods

被引：0
|
作者：
Li, M. [1 ]
Liu, H. [2 ]
Ning, Z. [2 ]
Ren, J. [1 ]
Tang, H. [1 ]
Yu, D. [2 ]
Eliseev, S. [3 ,4 ]
Kudryavtsev, A. [3 ,4 ]
机构：
[1] School of Astronautics, Beihang University, Beijing, China
[2] Plasma Propulsion Laboratory, Harbin Institute of Technology, Harbin, China
[3] St. Petersburg State University, St. Petersburg, Russia
[4] ITMO University, 49 Kronverkskiy Ave., St. Petersburg,197101, Russia
来源：
High Temperature Material Processes | 2014年 / 18卷 / 1-2期
关键词：
Magnetoplasma - Electric potential - Ion bombardment - Cathodes - Electric discharges - Ionization of gases - Charged particles - Numerical methods;
D O I：
10.1615/HighTempMatProc.2015015355
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：83 / 90
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