Rchr
J-GLOBAL ID:201801015228016590   Update date: Dec. 29, 2020

Ozawa Kohei

オザワ コウヘイ | Ozawa Kohei
Affiliation and department:
Homepage URL  (1): http://www.mech.kyutech.ac.jp/rfd/ozawa_top.html
Research field  (1): Aerospace engineering
Research keywords  (4): Detonation ,  Hybrid Rocket ,  Combustion ,  Fluid Dynamics
Research theme for competitive and other funds  (10):
  • 2020 - 2021 Investigation on Boundary Layer Combustion of Liquefying Fuel with Low Viscosity in Acceleration Environment
  • 2020 - 2021 Study of Conductive Resin Mixed with Graphene for Upgrade of Solid Fuels Capable of Flow Rate Measurement
  • 2020 - 2021 Demonstration of Advanced Closed-Loop Thrust Control of Hybrid Rockets Using Additively-manufactured Solid Fuels
  • 2019 - 2021 Upgrade of Thruster for Nano-satellites Using Functional Solid Fuels Manufactured by a 3D Printer
  • 2018 - 2021 Investigation on Boundary Layer Combustion of Liquefying Fuel with Low Viscosity in Acceleration Environment
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Papers (10):
more...
MISC (21):
more...
Patents (1):
  • A manufacturing method of solid fuels for hybrid rocket engines with a real-time regression rate measurement function
Books (1):
  • Chemical Rocket Propulsion: A Comprehensive Survey of Energetic Materials
    Springer 2016 ISBN:9783319277462
Lectures and oral presentations  (28):
  • Accuracy of real-time fuel regression measurement function of a 3d printed solid fuel
    (AIAA Propulsion and Energy 2020 Forum 2020)
  • Real-time Regression Rate Measurement of an Additive-manufactured Functional Hybrid Rocket Fuel
    (Real-time Regression Rate Measurement of an Additive-manufactured Functional Hybrid Rocket Fuel 2019)
  • Combustion Flow of Wax-based Hybrid Rockets in Various Acceleration Environments
    (JST さくらサイエンスプラン 2019 年度 熱流体工学分野に関する国際共同セミナー 2019)
  • Boundary-Layer Combustion of Wax-based Fuels at Various Chamber Pressures under Two Static Acceleration Environments
    (AIAA Propulsion and Energy 2019 Forum 2019)
  • Investigation of Graphite Nozzle Erosion in Hybrid Rockets Using N2O/HDPE
    (AIAA Propulsion and Energy 2019 Forum 2019)
more...
Education (3):
  • 2014 - 2017 The University of Tokyo Doctoral Course, Department of Aeronautics and Astronautics
  • 2012 - 2014 The University of Tokyo Master Course, Department of Aeronautics and Astronautics
  • 2008 - 2012 The University of Tokyo Department of Aeronautics and Astronautics
Professional career (2):
  • 博士(工学) (東京大学)
  • Doctor of Engineering (The University of Tokyo)
Work history (2):
  • 2017/03/27 - 現在 Kyushu Institute of Technology Faculty of Engineering Department of Mechanical and Control Engineering Assistant Professor
  • 2015/04/01 - 2017/03/24 The University of Tokyo School of Engineering Special researcher of the Japan Society for the Promotion of Science
Committee career (1):
  • 2020/03 - 2021/02 The Japan Society for Aeronautical and Space Sciences West Branch Executive Secretary
Awards (2):
  • 2016/07 - AIAA AIAA Hybrid Rockets Best Student Paper Flight Performance Simulations of Vertical Launched Sounding Rockets Using Altering-Intensity Swirling-Oxidizer-Flow-Type Hybrid Motors
  • 2013/06/09 - Japanese Rocket Society Award
Association Membership(s) (5):
宇宙工学委員会 ,  Japan Explosives Society ,  The Japan Society for Aeronautical and Space Sciences ,  AIAA ,  JSME
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