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

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

Engineering education effects of the student rocket project at Fukuoka University

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

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

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
非爆発性ハイブリッドロケット用低融点燃料に関する研究
ハイブリッドロケット用低融点熱可塑性樹脂燃料の構成樹脂含有量が貯蔵弾性率に及ぼす影響
Experimental Study on Effect of Swirling Oxidizer Flow on Average and Local Regression Rate of Low-Melting-Point Thermoplastic Fuel for Hybrid Rockets
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に関する研究