Results 11 to 20 of about 6,632 (182)

In situ erosion measurement tools for electric propulsion thrusters: triangular laser head and telemicroscope

open access: yesEPJ Techniques and Instrumentation, 2022
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
doaj   +1 more source

Plume Divergence and Discharge Oscillations of an Accessible Low-Power Hall Effect Thruster

open access: yesApplied Sciences, 2021
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
doaj   +1 more source

Optimization of a Faraday Cup Collimator for Electric Propulsion Device Beam Study: Case of a Hall Thruster

open access: yesApplied Sciences, 2021
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
doaj   +1 more source

Mode Transitions in Hall Effect Thrusters [PDF]

open access: yes49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 2013
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

open access: yesАвіаційно-космічна техніка та технологія, 2017
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
doaj   +1 more source

Fluid simulation on effect of background magnetic field on plasma characteristics in a Hall thruster

open access: yesAIP Advances, 2022
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
doaj   +1 more source

Investigating the neutralizer cathode location in the SPT type Hall Effect thruster [PDF]

open access: yesعلوم، فناوری و کاربردهای فضایی
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
doaj   +1 more source

Optimization of the E×B method for studying the charge composition of ions in the plasma jet of Hall effect thrusters [PDF]

open access: yesОмский научный вестник: Серия "Авиационно-ракетное и энергетическое машиностроение"
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
doaj   +1 more source

Numerical Aspects of Particle-in-Cell Simulations for Plasma-Motion Modeling of Electric Thrusters

open access: yesAerospace, 2021
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
doaj   +1 more source

Triple Langmuir Probes Measurements of LaB6 Hollow Cathodes Plume

open access: yesFrontiers in Physics, 2019
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
doaj   +1 more source

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