Development and Performance Test of a 50 W-class Hall thruster

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dc.contributor.authorLee, Donghoko
dc.contributor.authorKim, Holakko
dc.contributor.authorLee, Seunghunko
dc.contributor.authorDoh, Guentaeko
dc.contributor.authorChoe, Wonhoko
dc.date.accessioned2020-07-18T01:05:04Z-
dc.date.available2020-07-18T01:05:04Z-
dc.date.created2020-06-15-
dc.date.issued2019-09-18-
dc.identifier.citation36th International Electric Propulsion Conference (IEPC)-
dc.identifier.urihttp://hdl.handle.net/10203/275527-
dc.description.abstractA 50 W-class Hall thruster was developed and its performance was evaluated. The combination of a permanent magnet and electromagnet was utilized to produce magnetic fields. The developed thruster showed stable operation in the power range 42–74 W with anode voltage of 160–280 V. The measured values of thrust, specific impulse, and anode efficiency are 2.6 mN, 817 s, and 20%, respectively, at 52 W anode power. Current and propellant efficiencies are 0.59–0.65 and 0.55–0.63, respectively, in this power range.-
dc.languageEnglish-
dc.publisherUniversity of Vienna-
dc.titleDevelopment and Performance Test of a 50 W-class Hall thruster-
dc.typeConference-
dc.type.rimsCONF-
dc.citation.publicationname36th International Electric Propulsion Conference (IEPC)-
dc.identifier.conferencecountryAU-
dc.identifier.conferencelocationUniversity of Vienna, Main Building-
dc.contributor.localauthorChoe, Wonho-
dc.contributor.nonIdAuthorLee, Dongho-
dc.contributor.nonIdAuthorKim, Holak-
dc.contributor.nonIdAuthorLee, Seunghun-
dc.contributor.nonIdAuthorDoh, Guentae-
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NE-Conference Papers(학술회의논문)
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