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 R ⃝ HET magnetic circuit in order to obtain a new "Low-Erosion" magnetic configuration.
CITATION STYLE
ROSSI, A., MESSINE, F., & HENAUX, C. (2016). Parametric Optimization of a Hall Effect Thruster Magnetic Circuit. TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN, 14(ists30), Pb_197-Pb_202. https://doi.org/10.2322/tastj.14.pb_197
Mendeley helps you to discover research relevant for your work.