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dc.contributor.advisor이주-
dc.contributor.author양정수-
dc.date.accessioned2020-02-12T16:38:41Z-
dc.date.available2020-02-12T16:38:41Z-
dc.date.issued2017-02-
dc.identifier.urihttps://repository.hanyang.ac.kr/handle/20.500.11754/124049-
dc.identifier.urihttp://hanyang.dcollection.net/common/orgView/200000429505en_US
dc.description.abstractThis research proposes to change oil-pressure system to electro-mechanical system which is adapted thrust-vector control(TVC) system. The goal is to convert the existing hydraulic system of launchers to electro-mechanical system. And this paper, as part of project, studies FEM design of motor in electromagnetic system and EMF-Thermal coupled analysis was performed through simulation. In addition, this paper attempts to demonstrate the thermal reliability of motor operation in space through suggested limits of its hypotheses. So this paper focuses on lightening motor and the heat problem which is most common problem in motor operation.-
dc.publisher한양대학교-
dc.titleA Study on High Power Density Electric Motor Design for the Electrical Thrust Vector Control System of Launcher Vehicle-
dc.title.alternative전동식 발사체 추력벡터제어용 고출력밀도 전동기 형상설계-
dc.typeTheses-
dc.contributor.googleauthor양정수-
dc.contributor.alternativeauthorYang Jungsoo-
dc.sector.campusS-
dc.sector.daehak대학원-
dc.sector.department전기공학과-
dc.description.degreeMaster-
dc.contributor.affiliation전동기 설계 및 제어-
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GRADUATE SCHOOL[S](대학원) > ELECTRICAL ENGINEERING(전기공학과) > Theses (Master)
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