Skip to Main content Skip to Navigation
New interface
Journal articles

ID-HALL, a new double stage Hall thruster design. I. Principle and hybrid model of ID-HALL

Abstract : In Hall thrusters, ions are extracted from a quasineutral plasma by the electric field induced by the local drop of electron conductivity associated with the presence of a magnetic barrier. Since the electric field is used both to extract and accelerate ions and to generate the plasma, thrust and specific impulse are not independent in a Hall thruster. There is a need for versatile thrusters that can be used for a variety of maneuvers, i.e., that can operate either at high thrust or at high specific impulse for a given power. The double stage Hall thruster (DSHT) design could allow a separate control of ionization and acceleration, and hence separate control of thrust and specific impulse. In the DSHT configuration, a supplementary plasma source (ionization stage), independent of the applied voltage, is added and placed upstream of the magnetic barrier (acceleration stage). The DSHT concept is also well adapted to the use of alternative propellants, lighter and with a less efficient ionization than xenon. Several designs of double stage Hall thrusters have been proposed in the past, but these attempts were not really successful. In this paper, we present a brief review of the main DSHT designs described in the literature, we discuss the relevance of the DSHT concept, and, on the basis of simple physics arguments and simulation results, we propose a new design, called ID-HALL (Inductive Double stage HALL thruster). In this design, the ionization stage is a magnetized inductively coupled RF plasma. The inductive coil is inside the central cylinder of the thruster and located nearby the acceleration stage. Preliminary modeling results of this DSHT are described. Published by AIP Publishing. https://doi.
Complete list of metadata

Cited literature [30 references]  Display  Hide  Download

https://hal.archives-ouvertes.fr/hal-02326140
Contributor : Laurent Garrigues Connect in order to contact the contributor
Submitted on : Tuesday, October 22, 2019 - 2:25:15 PM
Last modification on : Monday, July 4, 2022 - 10:25:01 AM
Long-term archiving on: : Thursday, January 23, 2020 - 6:43:40 PM

File

PhysPlasmas_25_093503.pdf
Publisher files allowed on an open archive

Identifiers

Citation

Loic Dubois, F. Gaboriau, Laurent Liard, Dominique Harribey, Carole Hénaux, et al.. ID-HALL, a new double stage Hall thruster design. I. Principle and hybrid model of ID-HALL. Physics of Plasmas, 2018, 25 (9), pp.093503. ⟨10.1063/1.5043354⟩. ⟨hal-02326140⟩

Share

Metrics

Record views

69

Files downloads

99