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]
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
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]
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
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]
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
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
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
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
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]
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

