DC Field | Value | Language |
---|---|---|
dc.contributor.advisor | 최원호 | - |
dc.contributor.author | Park, Dongha | - |
dc.contributor.author | 박동하 | - |
dc.date.accessioned | 2024-07-30T19:31:21Z | - |
dc.date.available | 2024-07-30T19:31:21Z | - |
dc.date.issued | 2024 | - |
dc.identifier.uri | http://library.kaist.ac.kr/search/detail/view.do?bibCtrlNo=1096779&flag=dissertation | en_US |
dc.identifier.uri | http://hdl.handle.net/10203/321561 | - |
dc.description | 학위논문(석사) - 한국과학기술원 : 원자력및양자공학과, 2024.2,[v, 47 p. :] | - |
dc.description.abstract | Hall thrusters are electric propulsion systems employed in various space missions for their high thrust-to-power ratio and specific impulse. Accurate thrust measurement of Hall thrusters is essential for estimating key performance indicators such as thrust, specific impulse, and efficiency. This study developed a thrust stand using a load cell to measure the thrust more simply and easily. The sensitivity and uncertainty of the measurement system were estimated through calibration with known weights, and this method was applied to measure the thrust of a 20 mN-class Hall thruster. The results obtained from the load cell were then compared with those measured using a Position Sensitive Detector (PSD). | - |
dc.language | eng | - |
dc.publisher | 한국과학기술원 | - |
dc.subject | 홀추력기▼a추력측정▼a추력스탠드▼a로드셀 | - |
dc.subject | Hall thruster▼aThrust measurement▼aThrust stand▼aLoad cell | - |
dc.title | Development of a prototype load cell based thrust measurement system for 200 mN-class hall thrusters | - |
dc.title.alternative | 200 mN급 홀추력기 추력 측정을 위한 로드셀 기반의 프로토타입 추력측정장치 개발 | - |
dc.type | Thesis(Master) | - |
dc.identifier.CNRN | 325007 | - |
dc.description.department | 한국과학기술원 :원자력및양자공학과, | - |
dc.contributor.alternativeauthor | Choe, Wonho | - |
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