TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
Online ISSN : 1884-0485
ISSN-L : 1884-0485
b) Electric and Advanced Propulsion : Joint session with 34th IEPC
Parametric Optimization of a Hall Effect Thruster Magnetic Circuit
Alberto ROSSIFrédéric MESSINECarole HENAUX
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2016 Volume 14 Issue ists30 Pages Pb_197-Pb_202

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Abstract

A Hall effect thruster (HET) incorporates a magnetic circuit that must generate a specific flux density spatial distribution inside and near the outlets of the plasma channel. The first objective of the design process of this type of structure is to obtain a specific magnetic filed topology in the thruster channel by fixing radial and axial components of the magnetic field and a certain inclination of magnetic flux lines. The aim of this work is to develop a tool for solving this inverse magneto static problem, which is applied to the SNECMA PPS1350 ® HET magnetic circuit in order to obtain a new “Low-Erosion” magnetic configuration.

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© 2016 The Japan Society for Aeronautical and Space Sciences
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