Radio-Frequency Ion Thruster with Additional Magnetic Field: Experimental Investigation
- Авторлар: Melnikov A.V.1, Khartov S.A.1
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Мекемелер:
- Moscow Aviation Institute (National Research University)
- Шығарылым: Том 65, № 13 (2018)
- Беттер: 980-985
- Бөлім: Article
- URL: https://journals.rcsi.science/0040-6015/article/view/173137
- DOI: https://doi.org/10.1134/S0040601518130086
- ID: 173137
Дәйексөз келтіру
Аннотация
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.
Негізгі сөздер
Авторлар туралы
A. Melnikov
Moscow Aviation Institute (National Research University)
Хат алмасуға жауапты Автор.
Email: k208@mai.ru
Ресей, Moscow, 125993
S. Khartov
Moscow Aviation Institute (National Research University)
Email: k208@mai.ru
Ресей, Moscow, 125993
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