Photograph

Name
YONEMOTO Koichi
Affiliation
Faculty of Engineering
Department of Mechanical and Control Engineering
Title
Professor
Birthday
1953.07.28
Laboratory address
1-1 Sensui-cho,Tobata-ku, Kitakyushu,Fukuoka,804-8550 Japan
Laboratory telephone number
+81-93-884-3179
Web Site
http://www.mech.kyutech.ac.jp/yonemoto/
E-mail address
E-mail address
Research areas, keyword
Reusable Space Transportation System, Mars Exploration Aircraft
School Attended (except graduate school)
  • Tohoku University , Faculty of Engineering , Department of Mechanical Engineering

    University , 1977.03 , Graduated , JAPAN

Graduate School Attended, etc.
  • The University of Tokyo , Graduate School, Division of Engineering , Mechanical Engineering

    Master Course , 1980.03 , Completed , JAPAN

Degree
  • Doctor of Engineering , Aerospace engineering , The University of Tokyo , Thesis , 1988.04

Employment Record in Research
  • Department of Mechanical and Control Engineering, Faculty of Engineering, Kyushu Institute of Technology, Professor, 2008.04 -

External Career
  • Kawasaki Heavy Industries Ltd., Aerospace Company , Researcher , 1980.04 - 2005.04

Academic Society Joined
  • The Japan Society of Mechanical Engineers , 2007.02 - , JAPAN

  • Japan Aerospace Technology Foundation (General Icorprated Association) , 1998.04 - 1999.03 , JAPAN

  • American Institute of Aeronautics and Astronautics , 1990.04 - , JAPAN

Research Field (grants-in-aid-for-scientific-research classification)
  • Aerospace engineering

Research Field (ReaD classification)
  • Rockets, missiles

  • Space crafts

  • Aircraft

Research Career
  • Research and Development of Experimental Winged Rocket , 2007.04 -

    future space transportation system, reusable winged rocket , Aerospace engineering , Rockets, missiles , System and control engineering in general , Collaboration in Japan , Funded Research

  • Research on the Separation Vortex Structure at Ultra Low Reynolds Number and its Application to the Design of Lifting Surface of Mars Flight Exploration System , 2007.04 -

    Mars Flight Exploration System, Aerodynamic Characteristics of Very Low Reynolds Number , Aerospace engineering , Space crafts , Fluid mechanics in general , Collaboration in Japan , Grant-in-Aid for Scientific Research

  • Research and Development of New Carbon Fiber Reinforced Plastic with High Hydrogen Gas Barrier Capability , 2007.04 -

    Carbon Fiber Reinforced Plastic, hydrogen gas barrier capability , Aerospace engineering , Rockets, missiles , Testing of other materials , Collaboration in Japan , Cooperative Research

Published papers (2006.4〜)
  • Japanese , Aerodynamic Data Acquisition of Mars Airplane by High Altitude Flight Test , JAXA Research and Development Report , vol.JAXA-RR-16-00870 (p.69 - 80) , 2017.03 , Oyama A., Nagai H., Tokutake H., Fujita K., Anyoji M., Toyota H., Miyazawa Y., Yonemoto K., Okamoto M., Nonomura T., Motoda T., Takeuchi S., Kamata Y., Otshuki M., Asai K., Fujii K.

    DOI:info:doi/10.20637/JAXA-RR-16-008/0004, Others , The Multiple Authorship , Aerospace engineering

  • English , Stability Analysis of Nonlinear Dynamic Inversion Controller Applied to Winged Rocket , Transaction of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan , vol.14 (ists30) (p.9 - 16) , 2016.11 , Yamasaki H., Yonemoto K., Itakura K., Gossamsetti G.S., Ichige M., URA Y.

    Academic Journal , The Multiple Authorship , Aerospace engineering

  • English , Variable Pressure Wind Tunnel Test of Airfoils at Low Reynolds Numbers Designed for Mars Exploration Aircraft , Transaction of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan , vol.14 (ists30) (p.29 - 24) , 2016.09 , Tsukamoto H., Yonemoto K., Makizono T., Sasaki G., Tanaka K., Ikeda K., OchiH.

    Academic Journal , The Multiple Authorship , Aerospace engineering

  • English , Winged Test Rocket with Fully Autonomous Guidance and Control for Realizing Reusable Suborbital Vehicle , International Journal of Mechanical, Aerospace, Industrial, Mechatronic and Manufacturing Engineering , vol.10 (1) (p.96 - 107) , 2016.01 , Yonemoto K., Yamasaki H., Ichige M., Ura Y., Gossamsetti Guna S., Ohki T., Shirakata K., Choudhuri Ahsan R., Ishimoto S., Mugitani T., Asakawa H., Nanri H.

    Academic Journal , The Multiple Authorship

  • English , Stability Analysis of Nonlinear Dynamic Inversion Controller Applied to Winged Rocket , TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN , vol.14 (30) (p.Pg_9 - Pg_16) , 2016.01 , YAMASAKI Hiroshi, YONEMOTO Koichi, ITAKURA Kyoshiro, GOSSAMSETTI Guna Surendra, ICHIGE Masatomo, URA Yusuke

    DOI:10.2322/tastj.14.Pg_9, Academic Journal , The Multiple Authorship

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Research Achievement (Review)
  • Japanese , Super Pressure Hydrogen Gas Composite Tank Using Clay Film with High Gas Barrier Characteristics , The Japan Plastics Industry Federation , Plastics , vol.63 (8) (p.21 - 25) , 2012.08 , Yamamoto M., Hanaoka K., Nakano M., Shohara F., Yonemoto K., Yoshimitsu Y.

    The Commerce Magazine , The Multiple Authorship

  • Japanese , Education of Project-Leader-Type Doctor Engineer , Meisen Corporation , Meisen Magazine (859) (p.1 - 4) , 2012.07 , Yonemoto K.

    Others , The Simple Work

  • Japanese , (20) , 2012.04

    Others , The Simple Work , Aerospace engineering

Industrial Property
  • The Patent , High Pressure Gas Container and Its Manufacturing Method , Yamamoto M., Yoshimitsu Y., Yonemoto K., Imai T.

    Patent application number ( 6000618 , 2016.09.09 ) Registration-of-patent number ( 6000618 , 2016.09.09 ) , JAPAN , Existence , Composite materials/physical properties , Aerospace engineering

  • The Patent , Flight Control Mechanism of Parafoil , Yonemoto, K., Fujie, S., Hoshino, M., Nakamura, T., Oshikata, Y., Kaji, S.

    Patent application number ( '2006-301071 , 2006.11.07 ) Registration-of-patent number ( 4945752 , 2012.03.16 ) , JAPAN , Existence , Aerospace engineering

  • The Patent , Carbon Fiber Reinforced Prepreg of Gas Barrier Properties, Carbon Fiber Reinforced Plastics and Method of Producing the Same , Koichi Yonemoto, Takeo Ebina, Fujio Mizukami, Keiichi Okuyama, Shoji Kamiya

    Patent application number ( 12/741,553 , 2008.10.27 ) Registration-of-patent number ( US 7,981,500 B2 , 2011.07.19 ) , JAPAN , Existence , Composite materials/physical properties

Research presentations (2006.4〜)
  • 31st International Symposium on Space Technology and Science, International Conference without screening , 2017.06 , Flight Control Stability of Multi-Hierarchy Dynamic Inversion for Winged Rocket , The Oral (generality) , Aerospace engineering

  • 31st International Symposium on Space Technology and Science, International Conference without screening , 2017.06 , Mars Airplane Balloon Experiment , The Oral (generality) , Aerospace engineering

  • 31st International Symposium on Space Technology and Science, International Conference without screening , 2017.06 , Conceptual Design Optimization of Several Types of Fully Reusable Winged Launch Vehicles , The Oral (generality) , Aerospace engineering

  • 31st International Symposium on Space Technology and Science, International Conference without screening , 2017.06 , Detailed Design Status of Experimental Winged Rocket WIRES#015 with Liquid Methane Engine , The Oral (generality) , Aerospace engineering

  • 31st International Symposium on Space Technology and Science, International Conference without screening , 2017.06 , Flight Test Result of Experimental Winged Rocket WIRES#014-3A , The Oral (generality) , Aerospace engineering

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Activities, such as a society and a committee
  • The Japan Society of Mechanical Engineers , Fellow Award Reviewer , 2007.03

  • Japan Aerospace Technology Foundation (General Icorprated Association) , Study and Research Committee of System Technology for Reusable Rocket: Member , 1998.04 - 1999.03

Past of Commissioned Research
  • Research on Reusable Sub-orbital Flight Demonstration System , 2012.09 - 2013.03 , The General Consignment Study

  • Research on the Flight Adaptive Optimal Guidance and Control System (Part 2) , 2009.11 - 2010.03 , The General Consignment Study

  • Research on Ceramic Compound CFRP (Carbon Fiber Reinforced Plastics) for Liquid Hydrogen Tank , 2008.10 - 2009.03 , The General Consignment Study

  • Research on the Flight Adaptive Optimal Guidance and Control System , 2008.08 - 2009.03 , The General Consignment Study

  • Elemental Composite Material Tests for Development of Liquid Hydrogen Tank , 2007.12 - 2008.03 , The General Consignment Study

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Past of Cooperative Research
  • Material Development of Composite Cryogenic Oxygen Tank , 2015.04 - 2018.03 , Cooperative Research within Japan

  • Research on Prototype Development of Cryogenic Oxygen Tank Made of Carbon Fiber Reinforced Plastic for Highly Frequent Operation, Part 4 , 2015.01 - 2015.03 , Cooperative Research within Japan

  • Conceptual Design of Sub-scaled Winged Test Rocket for Critical Technology Demonstration , 2014.12 - 2015.03 , Cooperative Research within Japan

  • Research on Guidance and Control of Sub-orbital Space Transportation System, Part A , 2013.12 - 2014.03 , Cooperative Research within an Affiliated University or Institute

  • Research on Conceptual Vehicle Design of Sub-orbital Space Transportation System , 2013.12 - 2014.03 , Cooperative Research within an Affiliated University or Institute

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Updated on 2018/05/09