Simulation of plasma detachment in VASIMR
Simulation of plasma detachment in VASIMR
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VASIMR 中等离子体脱离的模拟
DOI：
10.2514/6.2002-346
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发表时间：
2002
期刊：
影响因子：
--
通讯作者：
M. Carter
中科院分区：
文献类型：
--
作者：
A. Ilin;F. Chan;J. Squire;A. Tarditi;B. Breizman;M. Carter
等离子体排气的分离是磁性喷嘴操作的基本要素，需要实验、分析和计算机模拟研究。本文对变比冲磁等离子体火箭的等离子体分离过程进行了计算机模拟。粒子模拟和MHD方法已被使用，结果在本文中报告。
Detachment of the plasma exhaust is an essential element of a magnetic nozzle operation that requires experimental, analytic and computer simulation studies. The present work is devoted to computer simulations of the plasma detachment in the Variable Specific Impulse Magnetoplasma Rocket. Both particle simulation and MHD methods have been used and results are reported in this paper.