Radio-Frequency Ion Thruster with Additional Magnetic Field: Experimental Investigation
- 作者: Melnikov A.V.1, Khartov S.A.1
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隶属关系:
- Moscow Aviation Institute (National Research University)
- 期: 卷 65, 编号 13 (2018)
- 页面: 980-985
- 栏目: Article
- URL: https://journals.rcsi.science/0040-6015/article/view/173137
- DOI: https://doi.org/10.1134/S0040601518130086
- ID: 173137
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详细
Performances of a radio-frequency ion thruster with an additional external magnetic field in the area of the high-frequency discharge are experimentally investigated and the results of the investigation are presented. The calculated distribution of a magnetic field generated by an additional magnetic system for the current in the winding 1 A is given. How an additional external magnetic field influences on the ion current is examined. Performances of a laboratory model of a radio-frequency ion thruster with and without a constant external magnetic field are compared. Modes of thruster operation and current values in a magnetic system’s windings under which the increment of ion current is minimal are determined.
作者简介
A. Melnikov
Moscow Aviation Institute (National Research University)
编辑信件的主要联系方式.
Email: k208@mai.ru
俄罗斯联邦, Moscow, 125993
S. Khartov
Moscow Aviation Institute (National Research University)
Email: k208@mai.ru
俄罗斯联邦, Moscow, 125993
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