DC Field | Value | Language |
---|---|---|
dc.contributor.author | Lee, Dongho | ko |
dc.contributor.author | Kim, Holak | ko |
dc.contributor.author | Lee, Seunghun | ko |
dc.contributor.author | Doh, Guentae | ko |
dc.contributor.author | Choe, Wonho | ko |
dc.date.accessioned | 2020-07-18T01:05:04Z | - |
dc.date.available | 2020-07-18T01:05:04Z | - |
dc.date.created | 2020-06-15 | - |
dc.date.issued | 2019-09-18 | - |
dc.identifier.citation | 36th International Electric Propulsion Conference (IEPC) | - |
dc.identifier.uri | http://hdl.handle.net/10203/275527 | - |
dc.description.abstract | A 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.language | English | - |
dc.publisher | University of Vienna | - |
dc.title | Development and Performance Test of a 50 W-class Hall thruster | - |
dc.type | Conference | - |
dc.type.rims | CONF | - |
dc.citation.publicationname | 36th International Electric Propulsion Conference (IEPC) | - |
dc.identifier.conferencecountry | AU | - |
dc.identifier.conferencelocation | University of Vienna, Main Building | - |
dc.contributor.localauthor | Choe, Wonho | - |
dc.contributor.nonIdAuthor | Lee, Dongho | - |
dc.contributor.nonIdAuthor | Kim, Holak | - |
dc.contributor.nonIdAuthor | Lee, Seunghun | - |
dc.contributor.nonIdAuthor | Doh, Guentae | - |
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