摘要
Experimental study was carried out on the ion thruster plume thermal effect within the scope of thruster exit radius of 500, 700mm and 900mm, the angle of 0°-15° (assuming the thruster exit plane as the center of the circle, thruster exit axis as 0°) with the help of the heat flux sensor. PIC-DSMC (particle in cell direct simulation of Monte Carlo) algorithm was used to simulate the experimental conditions under different adaptation coefficients. The results showed that the adaptation coefficient of keV energy Xe particles to the surface (copper) of the heat flow sensor was close to 1.
| 投稿的翻译标题 | Adaptation coefficient of keV energy Xe particles to copper surface in Maxwell model |
|---|---|
| 源语言 | 繁体中文 |
| 页(从-至) | 2216-2222 |
| 页数 | 7 |
| 期刊 | Hangkong Dongli Xuebao/Journal of Aerospace Power |
| 卷 | 35 |
| 期 | 10 |
| DOI | |
| 出版状态 | 已出版 - 10月 2020 |
关键词
- Adaptation coefficient
- Electric propulsion plume
- Heat flux distribution
- Maxwell model
- Particle wall interaction
学术指纹
探究 'Maxwell模型中keV能量的Xe粒子对铜表面的适应系数' 的科研主题。它们共同构成独一无二的学术指纹。引用此
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