中国物理B ›› 2025, Vol. 34 ›› Issue (2): 25202-025202.doi: 10.1088/1674-1056/ad9e9b
Cheng Zhou(周成)1,2,3, Peng Wu(吴鹏)3, Yun-Tao Song(宋云涛)1,2, Jin-Xing Zheng(郑金星)1,2, Yong Li(李永)3,†, Ge Wang(王戈)3, and Hai-Yang Liu(刘海洋)2
Cheng Zhou(周成)1,2,3, Peng Wu(吴鹏)3, Yun-Tao Song(宋云涛)1,2, Jin-Xing Zheng(郑金星)1,2, Yong Li(李永)3,†, Ge Wang(王戈)3, and Hai-Yang Liu(刘海洋)2
摘要: The magnetoplasmadynamic thruster (MPDT) is characterized by its high specific impulse and substantial thrust density, making it a promising propulsion system for deep space exploration missions. In both laboratory experiments and practical applications, cathode ablation has emerged as a critical concern. An optical diagnostic approach based on monochromatic radiation temperature measurement, utilizing plume emission spectra and the selection of an appropriate test band, has been successfully employed. This method provides an accurate temperature distribution across the cathode surface, offering a novel testing technique for the optimization and evaluation of magnetic plasma thruster designs.
中图分类号: (Ion and plasma propulsion)