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Computation of Hall Thruster Performance

Journal of Propulsion and Power, 2001
A quasi-neutral one-dimensional hybrid model of a stationary plasma thruster has been used to predict the performance of a laboratory model thruster tested in the Propulsion Ionique pour Vols Orbitaux, Interpretation et Nouvelles Experiences, facility. In this model ions are treated as particles and electrons as a  uid and quasi neutrality is assumed ...
L. Garrigues, I. D. Boyd, J. P. Boeuf
openaire   +1 more source

µ-Hall Effect Thruster Characterization

49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 2011
Results of two methods to characterize a novel micro-Hall effect thruster are presented. The voltage-current characteristics of the thruster during steady state operation are reported. The exhaust plume is characterized using Faraday probe measurements and the beam efficiency is reported.
John-David de La Harpe   +4 more
openaire   +1 more source

Numerical modeling of Hall thruster

AIP Conference Proceedings, 2005
A stationary plasma thruster is numerically studied using different levels. An one dimensional modeling is first analyzed and compared with experimental results. A simplified model of oscillations thruster is proposed and used to control the amplitude of oscillations. A two dimensional numerical method is discussed and applied to the computation of the
openaire   +1 more source

Hall thruster-cathode coupling

35th Joint Propulsion Conference and Exhibit, 1999
Dennis Tilley   +2 more
openaire   +1 more source

The origin of the breathing mode in Hall thrusters and its stabilization

Journal of Applied Physics, 2021
Trevor Lafleur   +2 more
exaly  

On the mechanism of ionization oscillations in Hall thrusters

Journal of Applied Physics, 2021
Oleksandr Chapurin   +2 more
exaly  

Channel length and thruster performance of Hall thrusters

32nd Joint Propulsion Conference and Exhibit, 1996
Kimiya Komurasaki   +2 more
openaire   +1 more source

Performance enhancement of Hall Effect Thrusters using radiofrequency excitation

Acta Astronautica, 2022
Jesús Manuel Muñoz Tejeda   +2 more
exaly  

End-hall thrusters

21st International Electric Propulsion Conference, 1990
openaire   +1 more source

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