TAKAO Yoshinori

Organization

Faculty of Engineering, Division of Systems Research

Title

Associate Professor

Research Fields, Keywords

Electric Propulsion, Plasma Application

Mail Address

E-mail address

Homepage URL

http://www.takao-lab.ynu.ac.jp



写真a

Graduating School 【 display / non-display

  • 1998.04
    -
    2002.03

    Kyoto University   Faculty of Engineering   Graduated

Graduate School 【 display / non-display

  • 2004.04
    -
    2007.03

    Kyoto University  Graduate School, Division of Engineering  Department of Aeronautics and Astronautics  Doctor Course  Completed

  • 2002.04
    -
    2004.03

    Kyoto University  Graduate School, Division of Engineering  Department of Aeronautics and Astronautics  Master Course  Completed

External Career 【 display / non-display

  • 2018.04
    -
    2020.03

    Japan Aerospace Exploration Agency   Institute of Space and Astronautical Science   Visiting Associate Professor  

  • 2009.03
    -
    2014.03

    Kyoto University   Graduate School of Engineering, Department of Aeronautics and Astronautics   Assistant Professor  

  • 2007.04
    -
    2009.03

    THine Electronics,Inc.  

  • 2004.04
    -
    2007.03

    Japan Society for the Promotion of Science   Research Fellowship for Young Scientists of the Japan Society for the Promotion of Science  

Academic Society Affiliations 【 display / non-display

  • 2004
     
     
     

    The American Institute of Aeronautics and Astronautics

  • 2004
     
     
     

    The Japan Society for Aeronautical and Space Sciences

  • 2003
     
     
     

    The Japan Society of Applied Physics

Field of expertise (Grants-in-aid for Scientific Research classification) 【 display / non-display

  • Aerospace engineering

  • Plasma science

 

Thesis for a degree 【 display / non-display

  • Development of a Miniature Electrothermal Thruster Using Microwave-Excited Microplasmas for Ultra Small Satellites

    Y. Takao 

      2007.03  [Refereed]

    Doctoral Thesis   Single Work

  • 超小型推進機のためのマイクロプラズマ源とマイクロノズル流れの解析

    鷹尾 祥典 

      2004.03

    Master Thesis   Single Work

     View Summary

    京都大学大学院 工学研究科 航空宇宙工学専攻 超小型人工衛星の軌道・姿勢制御を用途としたマイクロ波励起マイクロプラズマスラスタを対象に、数値計算による性能見積もりを行った。解析にはマイクロプラズマ源とマイクロノズル流れを分けて行い、前者には体積平均モデルとマクスウェル方程式を利用し、後者には2温度モデルに基づくナビエ・ストークス方程式を利用した。分散関係式との比較により表面波の伝播を確認し、また、境界層が支配的なことから、ノズルの全長を短くすることが性能向上に望ましいと分かった。

Papers 【 display / non-display

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Review Papers 【 display / non-display

Academic Awards Received 【 display / non-display

  • The 78th JSAP Autumn Meeting 2017, Poster Award

    2017.10.01   Japan Society of Applied Physics(JSAP)   Fabrication of electrospray thrusters using Minimum System

    Winner: Masayoshi Nagao,Naoki Inoue,Yoshinori Takao,Nariyuki Tasumi,Katsuhisa Murakami,Sommawan Khumpang,Shiro Hara

Presentations 【 display / non-display

  • Particle Simulations of 1-cm Class Plasma Sources with Applied Magnetic Fields and Their Application to Space Propulsion

    Yoshinori Takao  [Invited]

    Plasma Conference 2017  2017.11  

  • 3D Particle Simulation for Electron Extraction Mechanisms of a Miniature Microwave Discharge Neutralizer

    Kenta Hiramoto, Yuichi Nakagawa, Hiroyuki Koizumi, and Kimiya Komurasaki, Yoshinori Takao

    Proceedings of the 52nd AIAA/SAE/ASEE Joint Propulsion Conference (Propulsion and Energy Forum),  (Salt Lake City, USA)  2016.07  

  • Validation of a 3D Particle Simulation Model for a Miniature Microwave Discharge Ion Thruster

    Yoshinori Takao, Koji Eriguchi, Kouichi Ono, Yuto Sugita, Hiroyuki Koizumi, and Kimiya Komurasaki

    Proceedings of the 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference (Propulsion and Energy Forum),  (Cleveland, USA)  2014.07  

  • Plasma Diagnostics in a Miniature Microwave Discharge Ion Thruster

    Y. Sugita, H.Koizumi, R. Tsukizaki, H. Kuninaka, Y. Takao, Y. Yamagiwa, M. Matsui

    Proceedings of the 33rd International Electric Propulsion Conference,  (Washington, D.C., USA)  2013.10  

  • Three-Dimensional Particle-in-Cell Simulation of a Miniature Microwave Discharge Ion Thruster µ1

    Y. Takao, K. Eriguchi, K. Ono, Y. Sugita, H. Koizumi, and K. Komurasaki

    Proceedings of the 33rd International Electric Propulsion Conference,   (Washington, D.C., USA)  2013.10  

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