Experimental and numerical characterization of the narrow channel Hall thruster discharge
Author:
Affiliation:
1. Faculty of Aerospace Engineering, Technion—Israel Institute of Technology, Haifa 3200003, Israel
Funder
Israeli Ministry of Innovation
Publisher
AIP Publishing
Subject
General Physics and Astronomy
Link
https://aip.scitation.org/doi/pdf/10.1063/5.0067264
Reference24 articles.
1. Modern Small Satellites-Changing the Economics of Space
2. The technological and commercial expansion of electric propulsion
3. Fundamental difference between the two Hall thruster variants
4. Attitude control: A key factor during the design of low-thrust propulsion for CubeSats
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1. Experimental investigation of an external discharge very low anode power (< 20 W) hall thruster;Journal of Electric Propulsion;2022-10-03
2. Physics of electric propulsion;Journal of Applied Physics;2022-09-21
3. Experimental Investigation of an External Discharge Very Low Power (<20W) Hall Thruster;2022-08-17
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