川端 洋

Kawabata Yo

  • 講師
  • 学位：博士（工学）

基本情報

所属

  • Undergraduate School of Engineering / Department of Aeronautics and Astronautics Aerospace Course
  • Graduate School of Engineering / Course of Mechanical Engineering

詳細情報

研究キーワード

  • Space propulsion
  • Hybrid rocket
  • Viscoelastic material
  • Combustion engineering

研究分野

  • Aerospace, marine, and maritime Engineering Aerospace engineering Aerospace engineering
  • Nanotechnology/Materials Polymer materials Polymer/Textile materials

受賞

  • 日本航空宇宙学会北部支部 日本航空宇宙学会北部支部2012年講演会「Best Presentation Award for student」 小型ハイブリッドロケット打ち上げ海上回収実験
  • 秋田大学 平成23年度秋田大学学長表彰奨励賞
  • 日本航空宇宙学会 第6回能代宇宙イベント日本航空宇宙学会北部支部特別賞 ポスター展最優秀賞(団体)

論文

Small Hybrid Rocket Launch Experiment During the 18th Noshiro Space Event

Measurement of the Fuel Regression Rate of a Hybrid Rocket Fuel in a Stagnation Point Combustion Chamber with Observation Windows

Engineering education effects of the student rocket project at Fukuoka University

VISCOELASTIC BEHAVIOR AND STRUCTURAL FEASIBILITY ANALYSIS OF LOW-MELTING-POINT THERMOPLASTIC FUEL FOR HYBRID ROCKETS

Influence of the Chemical Composition of Physical Properties of Low-Melting-Point Thermoplastics for Hybrid Rocket Fuel

Experimental and Numerical Study on Feasibility of 5 kN Thrust Level Hybrid Rocket Motor Using the Low-Melting-Point Thermoplastic Fuel

Experimental Study on 5 kN Thrust Level Hybrid Rocket Motor Using the Low-Melting-Point Thermoplastic Fuel

DEVELOPMENT OF A DIRECT INJECTION GAS-HYBRID ROCKET SYSTEM USING GLYCIDYL AZIDE POLYMER

IMPROVEMENT OF COMBUSTION EFFICIENCY USING A BAFFLE PLATE FOR A LT/GOX HYBRID ROCKET MOTOR

Development of a Candy Hybrid Rocket Motor for Undergraduate Space Education

Experimental Investigation of Fuel Regression Rate of Low-Melting-Point Thermoplastic Fuels in the Altering-Intensity Swirling-Oxidizer-Flow-Type Hybrid Rocket Engine

Observation of combustion behavior of lowmelting temperature fuel for a hybrid rocket using double slab motor

A study on Combustion Efficiency Improvement of Low Melting Temperature Thermoplastics as a Hybrid Rocket Fuel

講演・口頭発表等

  • Design and Development of Hybrid Rocket in Tokai University Student Rocket Project (Current Status of Unit H-60 and Prospects for Higher Altitude)
  • Study on Frequency Characteristics of Low Frequency Instabilities in 2D Slab Burner
  • A Small Hybrid Rocket Launch Experiment in 18th Noshiro Space Event
  • Developing a Stagnation Point Combustion Chamber and Measuring the Fuel Regression Rate of Hybrid Rocket Fuel
  • Experimental Investigation on the Scale Effect of Hybrid Rockets With a Low Melting Point Fuel
  • Fuel Regression Rate Measurement by Stagnation Point Combustor with Observation Window for Hybrid Rocket
  • A Study on the Scale Effect of Hybrid Rocket Using Paraffin Wax

担当経験のある科目

  • APPLIED MATHMATICS
  • UNDERGRADUATE RESEARCH 2
  • SEMINAR OF STUDIES ON MECHANICAL ENGINEERING 4
  • SEMINAR OF STUDIES ON MECHANICAL ENGINEERING 3
  • UNDERSTANDING LOCAL COMMUNITIES
  • AIRCRAFT PROPULSION
  • UNDERGRADUATE RESEARCH 1
  • AIRCRAFT MAINTENANCE APPLICATIONS
  • SEMINAR OF STUDIES ON MECHANICAL ENGINEERING 2
  • SPACE TECHNOLOGY
  • AEROSPACE LABORATORY EXERCISES 1
  • FRESHMAN SEMINAR (B)
  • AEROSPACE FRONTIER SCIENCE AND TECHNOLOGY
  • RESEARCH SEMINAR 1
  • SEMINAR OF STUDIES ON MECHANICAL ENGINEERING 1
  • AEROSPACE LABORATORY EXERCISES 2
  • AEROSPACE DRAFTING
  • ADVANCED SEMINAR
  • BASIC MECHANICAL ENGINEERING A
  • Fluid engineering I

所属学会

  • Japanese Rocket Society
  • NPO法人大学宇宙工学コンソーシアム(UNISEC)
  • Combustion Society of Japan
  • The Japan Society for Aeronautical and Space Sciences
  • The Japan Society of Mechanical Engineers
  • Japan Explosives Society

共同研究・競争的資金等の研究課題

観察窓付き淀み点燃焼器を用いたハイブリッドロケット用低融点燃料の燃焼モデル確立

イオン液体を用いた環境配慮型ロケット推進薬の合成と燃焼反応解析

福岡県産宇宙輸送サービスを目指した高性能ハイブリッドロケットエンジンと小型観測ロケット開発

観察窓付き端面燃焼器を用いたハイブリッドロケット用低融点燃料の溶融層流動現象観察(継続研究)

酸化剤旋回流が低融点燃料を用いたハイブリッドロケットの局所燃焼速度に与える影響の解明と福岡県産ロケットへの適用を目指した応用研究

低融点ポリマーブレンドの物性評価とハイブリッドロケット用燃料への応用

観察窓付き端面燃焼器を用いたハイブリッドロケット用低融点燃料の溶融層流動現象観察

低融点燃料を用いたハイブリッドロケットのスケール効果解明と福岡県内ロケット産業創出を目指した萌芽的研究

IMPROVEMENT OF COMBUSTION EFFICIENCY USING A BAFFLE PLATE FOR A LT/GOX HYBRID ROCKET MOTOR

メディア報道

  • 小型ロケットの打ち上げ実験に成功(福岡大学)
  • ぐるり関東 知ラナカッタYO!
  • 変ラボ 24時間耐久恐怖実験スペシャル
  • 秋大、学生団体で初成功
  • 秋大宇宙プロジェクト ロケット発射実験が成功
  • ハイブリッドロケット発射実験成功
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