Flash-over propagation simulation upon spacecrafts solar panels
JOURNAL OF APPLIED PHYSICS(2021)
摘要
A plasma expansion model is developed. It is used to compute flash-over propagation upon spacecraft solar panels. In order to take into consideration the plasma extinction, a cathode spot model is developed and coupled to a plasma expansion model. A minimum on the sheath potential has been found, and it explains the end of plasma emission by the cathode and, therefore, the end of the plasma expansion. Numerical results are compared with experimental measurements and are in good agreement with them. The model can be later used to prevent arcing on spacecrafts solar panels. Published under an exclusive license by AIP Publishing.
更多查看译文
关键词
propagation simulation,spacecrafts,solar,flash-over
AI 理解论文
溯源树
样例
![](https://originalfileserver.aminer.cn/sys/aminer/pubs/mrt_preview.jpeg)
生成溯源树,研究论文发展脉络
Chat Paper
正在生成论文摘要