Results 11 to 20 of about 8,678 (302)

Predicting Performance of Hall Effect Ion Source Using Machine Learning

open access: yesAdvanced Intelligent Systems
Accurate performance prediction methods are essential for the development of high‐efficiency Hall effect ion sources, which are employed in industries ranging from material surface treatment to spacecraft electric propulsion (known as Hall thrusters ...
Jaehong Park   +8 more
doaj   +2 more sources

An in-flight plasma diagnostic package for spacecraft with electric propulsion

open access: yesEPJ Techniques and Instrumentation, 2021
The plasma diagnostics presented in this article target the plasma surrounding a spacecraft that is created by the electric thruster and its surface modifying effects. The diagnostic package includes a retarding potential analyzer, a plane Langmuir probe,
Thomas Trottenberg   +15 more
doaj   +1 more source

Future Directions for Electric Propulsion Research

open access: yesAerospace, 2020
The research challenges for electric propulsion technologies are examined in the context of s-curve development cycles. It is shown that the need for research is driven both by the application as well as relative maturity of the technology.
Ethan Dale   +2 more
doaj   +1 more source

Monte Carlo modeling of low-energy electron-induced secondary electron emission yields in micro-architected boron nitride surfaces [PDF]

open access: yes, 2019
Surface erosion and secondary electron emission (SEE) have been identified as the most critical life-limiting factors in channel walls of Hall-effect thrusters for space propulsion.
Alvarado, Andrew   +3 more
core   +2 more sources

Temperature Gradient in Hall Thrusters [PDF]

open access: yesApplied Physics Letters, 2003
Plasma potentials and electron temperatures were deduced from emissive and cold floating probe measurements in a 2 kW Hall thruster, operated in the discharge voltage range of 200-400 V. An almost linear dependence of the electron temperature on the plasma potential was observed in the acceleration region of the thruster both inside and outside the ...
Staack, D., Raitses, Y., Fisch, N. J.
openaire   +3 more sources

Development of an indirect thrust stand based on a cantilever beam

open access: yesAIP Advances, 2021
There is a large number of missions that have been or will be launched soon that utilize the electric propulsion (EP), which is considered a key technology for applications in present and future space missions.
H. Zhang, D. T. Li, F. He, X. W. Chen
doaj   +1 more source

Experimental Verification of the Magnetic Field Topography inside a small Hall Thruster

open access: yesMeasurement Science Review, 2021
The magnetic circuit of a 500 W class Hall thruster, an electric propulsive device for spacecraft, was characterized experimentally and the results compared with simulation in order to verify the design.
Jakubczak Maciej   +2 more
doaj   +1 more source

An analytical review on electric Propulsion system for space satellites [PDF]

open access: yesINCAS Bulletin, 2020
This paper describes the latest advances in electric propulsion systems prepared for the new space exploration activity. Missions to the Moon and Mars will require these new thrusters to convey the huge amounts of provisions that would be expected to ...
Sourav BASU   +3 more
doaj   +1 more source

Hybrid-PIC Modeling of a High-Voltage, High-Specific-Impulse Hall Thruster [PDF]

open access: yes, 2013
The primary life-limiting mechanism of Hall thrusters is the sputter erosion of the discharge channel walls by high-energy propellant ions. Because of the difficulty involved in characterizing this erosion experimentally, many past efforts have focused ...
Boyd, Iain D.   +3 more
core   +2 more sources

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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