Development of the new BUSTLab Hall thruster with internal coaxial hollow cathode

dc.contributor.authorKokal, Ugur
dc.contributor.authorTuran, Nazli
dc.contributor.authorCelik, Murat
dc.contributor.authorKurt, Huseyin
dc.date.accessioned2025-05-10T15:21:37Z
dc.date.issued2017
dc.departmentİstanbul Medeniyet Üniversitesi
dc.description53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017 -- 10 July 2017 through 12 July 2017 -- Atlanta -- 195549
dc.description.abstractHK40 Hall thruster is a low power SPT-type Hall thruster with a boron nitride (BN) discharge channel of 40 mm in outer diameter. Based on the experience gained during the design and manufacturing of the HK40 Hall thruster, and the experiments that were conducted with this Hall thruster an advanced larger diameter Hall thruster with an LaB6 internal cathode is developed. In the design, protection of thruster wall material is aimed by the appropriate magnetic field inside the thruster channel. Design optimization of this new Hall thruster is made by investigating the effects of different design parameters, such as magnetic circuit and discharge channel geometry. A thermal model of this thruster is developed in order to investigate the heat distribution for the thruster-cathode system.
dc.description.sponsorshipIstanbul Medeniyet University Scientific Research Projects Support Fund, (F-UK-2015-710); Türkiye Bilimsel ve Teknolojik Araştirma Kurumu, TÜBITAK, (TUBITAK-112M862)
dc.identifier.doi10.2514/6.2017-4810
dc.identifier.isbn978-162410511-1
dc.identifier.scopus2-s2.0-85085405946
dc.identifier.scopusqualityN/A
dc.identifier.urihttps://doi.org/10.2514/6.2017-4810
dc.identifier.urihttps://hdl.handle.net/20.500.14730/6077
dc.indekslendigikaynakScopus
dc.language.isoen
dc.publisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
dc.relation.ispartof53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017
dc.relation.publicationcategoryKonferans Öğesi - Uluslararası - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.snmzKA_Scopus_20250302
dc.subjectCathodes; III-V semiconductors; Lanthanum compounds; Magnetic circuits; Propulsion; Design optimization; Design parameters; Discharge channel; Heat distribution; Hollow cathodes; Outer diameters; Thermal model; Wall materials; Hall thrusters
dc.titleDevelopment of the new BUSTLab Hall thruster with internal coaxial hollow cathode
dc.typeConference Object

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