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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

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

Temperature gradient in Hall thrusters [PDF]

open access: yesApplied Physics Letters, 2004
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 ...
D. Staack, Y. Raitses, N. J. Fisch
openaire   +3 more sources

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

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

Numerical and Experimental Investigation of Longitudinal Oscillations in Hall Thrusters

open access: yesAerospace, 2021
One of the main oscillatory modes found ubiquitously in Hall thrusters is the so-called breathing mode. This is recognized as a relatively low-frequency (10–30 kHz), longitudinal oscillation of the discharge current and plasma parameters.
Vittorio Giannetti   +4 more
doaj   +1 more source

The Application of Artificial Intelligent Algorithms in Electric Propulsion [PDF]

open access: yesHangkong bingqi
Electric propulsion technology has garnered significant attention due to its much higher specific impulse compared to traditional chemical propulsion. Currently, many mature on-orbit electric propulsion products have been developed worldwide.
Tian Bin, An Bingchen, Xie Kan, Yang Sulan
doaj   +1 more source

SITAEL HC1 Low-Current Hollow Cathode

open access: yesAerospace, 2020
SITAEL is active in the field of electric propulsion and is involved in the development of different thruster technologies—mainly Hall thrusters (HTs)—of power levels ranging from 100 W up to 20 kW.
Daniela Pedrini   +4 more
doaj   +1 more source

An Analysis of the Effect of Hall Thruster Plumes on Surface Charging of a Complex Spacecraft Structure

open access: yesApplied Sciences
This article aims to conduct an in-depth investigation into the environmental impact of Hall thruster plumes on spacecraft surface charging. The non-uniform plasma plume generated by Hall thrusters may trigger charging and discharging effects, making the
Xin Zhang   +11 more
doaj   +1 more source

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