Results 1 to 10 of about 169 (163)

Thirty percent conversion efficiency from radiofrequency power to thrust energy in a magnetic nozzle plasma thruster [PDF]

open access: yesScientific Reports, 2022
Innovations for terrestrial transportation technologies, e.g., cars, aircraft, and so on, have driven historical industries so far, and a similar breakthrough is now occurring in space owing to the successful development of electric propulsion devices ...
Kazunori Takahashi
doaj   +2 more sources

Small Hall Effect Thruster with 3D Printed Discharge Channel: Design and Thrust Measurements

open access: yesAerospace, 2021
This paper presents the design and performance of the UAH-78AM, a low-power small Hall effect thruster. The goal of this work is to assess the feasibility of using low-cost 3D printing to create functioning Hall thrusters, and study how 3D printing can ...
Kunning Xu, Wensheng Huang
exaly   +3 more sources

Stability of Wafer-Scale Thin Films of Vertically Aligned Hexagonal BN Nanosheets Exposed to High-Energy Ions and Reactive Atomic Oxygen [PDF]

open access: yesNanomaterials, 2022
Stability of advanced functional materials subjected to extreme conditions involving ion bombardment, radiation, or reactive chemicals is crucial for diverse applications.
Shiyong Huang   +9 more
doaj   +2 more sources

Numerical Modeling of Erosion in Hall Effect Thrusters

open access: yesParticles
The erosion of the accelerating chamber walls is one of the main factors limiting the operational life of Hall effect thrusters (HETs), and it is mainly related to the sputtering of ceramic walls due to the impacting energetic ion particles.
Matteo Passet   +2 more
doaj   +2 more sources

Simulation of Hollow Cathode in the Hall Thruster by Particle in Cell (PIC) Method [PDF]

open access: yesعلوم، فناوری و کاربردهای فضایی, 2023
The this article the characteristics of the hollow cathode plasma particles in the spt-100 hall effect thruster have been investigated by two-dimensional particle-in-cell simulation. One of the main and important components of the hall thruster is hollow
masumeh kiantaj   +3 more
doaj   +1 more source

Plume interference effects of the racetrack-shaped anode-layer Hall thruster system

open access: yesMechanical Engineering Journal, 2022
Plume interference effects on the discharge characteristics and thruster performance for two heads system were investigated to evaluate the optimum design of the Hall thruster cluster system using the anode-layer head.
Takeshi MIYASAKA   +6 more
doaj   +1 more source

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

Cathode effects in cylindrical Hall thrusters [PDF]

open access: yesJournal of Applied Physics, 2008
Stable operation of a cylindrical Hall thruster has been achieved using a hot wire cathode, which functions as a controllable electron emission source. It is shown that as the electron emission from the cathode increases with wire heating, the discharge current increases, the plasma plume angle reduces, and the ion energy distribution function shifts ...
E. M. Granstedt, Y. Raitses, N. J. Fisch
openaire   +3 more sources

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