An experimental study on the magnetic field permeability of an inductive-pulsed plasma thruster

被引:0
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作者
车碧轩
吴建军
程谋森
李小康
张宇
郭大伟
机构
[1] CollegeofAerospaceScienceandEngineering,NationalUniversityofDefenseTechnology
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中图分类号
V439.2 [];
学科分类号
摘要
Inductive-pulsed plasma thruster is an in-space propulsion device that generates thrust by ionizing and accelerating plasma through pulsed electromagnetic field. In this paper, the correlation between plasma structure evolution and magnetic field permeability is studied using a B-dot probe array system, combing with high-speed camera and electrical parameter measurement. Further discussions explained the mechanism how the magnetic permeation characteristics affect the energy deposition between circuit and plasma.
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页码:345 / 354
页数:10
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