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Issue title: Special Supplement Issue: Selected papers from the 13th International Workshop on Optimization and Inverse Problems in Electromagnetism (OIPE 2014)
Guest editors: Domenico Lahaye
Article type: Research Article
Authors: Rossi, Alberto* | Messine, Frédéric | Henaux, Carole
Affiliations: Groupe de Recherche en Electrodynamique-GREM3, Université de Toulouse, Toulouse, France
Correspondence: [*] Corresponding author: Alberto Rossi, Groupe de Recherche en Electrodynamique-GREM3, Université de Toulouse; INPT, UPS; LAPLACE (Laboratoire Plasma et Conversion d'Energie), UMR-CNRS 5213, ENSEEIHT, 2 rue Charles Camichel, BP 7122, F-31071 Toulouse cedex 7, France. E-mail:[email protected]
Abstract: Electrical propulsion in space is currently experiencing significant improvements. Among the electrical space propulsion technologies available, Hall effect thrusters work on the generation of plasma inside a cylindrical channel. These thrusters incorporate a magnetic circuit that has to generate a very specific magnetic mapping inside the plasma channel. There are mainly two objectives in the design process of this type of structure. The first objective is to obtain a specific magnetic mapping in the thruster channel with specific magnetic field radial component values. The second one is to obtain a specific magnetic field line inclination. Moreover, for spatial thrusters the minimization of the mass is one of the most important optimization criterion. The aim of this work is to develop a method for resolving the inverse magnetostatic problem, which is applied to obtain an optimized magnetic structure for Hall effect thrusters circuit.
Keywords: Hall effect thruster, parametric optimization, magnetic circuit
DOI: 10.3233/JAE-140158
Journal: International Journal of Applied Electromagnetics and Mechanics, vol. 53, no. S2, pp. S153-S165, 2017
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