KLI

EVALUATE OFTHE ION BEAM BEHAVIOR OF RADIO-FREQUENCY ION THRUSTER

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Abstract
Today, the application of satellite spatial propulsion using the practice of electric propulsion is quite common, including the success of the development of the hall and ion thruster. In 1884, Hittorf introduced for the first time a Radio Frequency Ion Thruster (RIT), which produced a plasma in a vacuum using a magnetic field. Inheriting his ideas and from the achievements of Applied Aerodynamics Research Laboratory, we study theoretical analysis Tool Development and measurement system. The system under research and development includes faraday probe, RPA probe and Torsional Thrust Stand with ion thruster and was tested with different input locations and conditions to evaluate the ion current density and ion energy distribution. The specifications of Faraday probe and RPA probe are designed based on the electronic density and temperature analysis, etc.
Author(s)
웬 티 투 흐엉
Issued Date
2021
Awarded Date
2021-08
Type
Dissertation
URI
https://oak.ulsan.ac.kr/handle/2021.oak/6000
http://ulsan.dcollection.net/common/orgView/200000503377
Alternative Author(s)
NGUYEN THI THU HUONG
Affiliation
울산대학교
Department
일반대학원 항공우주공학전공
Advisor
신지철
Degree
Master
Publisher
울산대학교 일반대학원 항공우주공학전공
Language
eng
Rights
울산대학교 논문은 저작권에 의해 보호받습니다.
Appears in Collections:
Aerospace Engineering > 1. Theses(Master)
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