Investigation of the Effect of Magnetic Field and Propellant on Hall Thruster’s Stability via a 0D Model

Investigation of the Effect of Magnetic Field and Propellant on Hall Thruster’s Stability via a 0D Model

Hall thrusters are plasma-based devices that have established themselves as one of the most attractive and mature electric propulsion technologies for space applications. These devices often operate in a regime characterized by low frequency, large amplitude oscillations of the discharge current, wh...

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Bibliographic Details
Main Authors: Luca Leporini, Ferhat Yaman, Tommaso Andreussi, Vittorio Giannetti
Format: Article
Language:English
Published: MDPI AG 2024-03-01
Series:Aerospace
Subjects:
electric propulsion
Hall thruster
plasma oscillations
breathing mode
ionization instability
alternative propellants
Online Access:https://www.mdpi.com/2226-4310/11/3/227

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