Results 11 to 20 of about 6,632 (182)
The lifetime of electric propulsion (EP) thrusters depends particularly on the erosion characteristics of operation relevant components, for instance, the grid hole erosion of gridded ion thrusters or the channel wall erosion of Hall effect thrusters ...
Carsten Bundesmann +8 more
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Plume Divergence and Discharge Oscillations of an Accessible Low-Power Hall Effect Thruster
Hall effect thrusters (HETs) are an increasingly utilized proportion of electric propulsion devices due to their high thrust-to-power ratio. To enable an accessible research thruster, our team used inexpensive materials and simplified structures to ...
Matthew Baird +3 more
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A Faraday cup (FC) is an instrument dedicated to current measurement in beams, jets and plasmas. It consists of a set of polarized electrodes mounted in such a way plasma sheath effect can be neglected, yielding accurate and reliable results.
Hugonnaud Valentin, Mazouffre Stéphane
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Mode Transitions in Hall Effect Thrusters [PDF]
Mode transitions have been commonly observed in Hall Effect Thruster (HET) operation where a small change in a thruster operating parameter such as discharge voltage, magnetic field or mass flow rate causes the thruster discharge current mean value and oscillation amplitude to increase significantly.
Sekerak, Michael J. +5 more
openaire +2 more sources
PROBE AND SPECTRAL INVESTIGATIONS OF ELECTRIC PROPULSION HALL EFFECT THRUSTER
The work is devoted to the study of a low-power Hall Effect Thruster. The currency of developing and increasing of integral characteristics of Hall Effect Thruster with power consumption less 0,3 kW is substantiated. The main directions of low-power Hall
Сергей Николаевич Кулагин
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Fluid simulation on effect of background magnetic field on plasma characteristics in a Hall thruster
Herein, the effect of the background magnetic field on plasma characteristics in a Hall thruster is numerically investigated using DUT-HTFS [Li et al., AIP Adv. 12, 015117 (2022)], an integrated fluid simulation platform on Hall thruster plasmas.
Nannan Li +3 more
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Investigating the neutralizer cathode location in the SPT type Hall Effect thruster [PDF]
The position of the cathode concerning the magnetic field map inside the discharge channel affects the performance and lifetime of the Hall effect thruster. The neutralizer cathode has two important functions in the Hall effect thruster.
mohammadmehdi shafie +4 more
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Optimization of the E×B method for studying the charge composition of ions in the plasma jet of Hall effect thrusters [PDF]
Electric propulsion rocket engines are widely used on board modern spacecraft. To ensure the efficient use of such engines, it is important to diagnose the plasma plume of the engine.
D. A. Maystrenko +3 more
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Numerical Aspects of Particle-in-Cell Simulations for Plasma-Motion Modeling of Electric Thrusters
The present work is focused on a detailed description of an in-house, particle-in-cell code developed by the authors, whose main aim is to perform highly accurate plasma simulations on an off-the-shelf computing platform in a relatively short ...
Giuseppe Gallo +6 more
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Triple Langmuir Probes Measurements of LaB6 Hollow Cathodes Plume
Lanthanum hexaboride hollow cathodes represent a viable option for high power Hall effect thruster applications, under development for the next generation of manned and robotic interplanetary missions.
Giulia Becatti +4 more
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