Personnel Information

写真a

Minato Ryojiro


The master's program in charge

Division of Production Systems Engineering

The department in charge

Department of Engineering

Job title

Assistant Professor

E-mail Address

E-mail address

Research field 【 display / non-display

  • Frontier Technology (Aerospace Engineering, Marine and Maritime Engineering) / Aerospace engineering

  • Air Breathing Propulsion

Keywords for Research Field 【 display / non-display

  • AirBreathing Engine

  • Reusable Space Vehicle, Supersonic and hypersonic aerodynamics, Space Propulsion

Graduate school・Graduate course, etc. 【 display / non-display

  • Tohoku University

    2002,Doctoral program,Graduate School, Division of Engineering,Division of Aeronautics and Space Engineering,Completed,Japan

Graduate school・major, etc. 【 display / non-display

  • Tohoku University

    1995,Faculty of Engineering,Department of Mechanical Electronics,Graduate,Japan

Degree 【 display / non-display

  • Doctor of Engineering

    Numerical Study of Ignition and Combustion by Plasma Torch in Supersonic Airflow

Academic Society 【 display / non-display

  • The Japan Society of Aeronautical ans Space Science

  • Combustion Society of Japan

  • The Japan Society of Mechanical Engineers

 
 

Books 【 display / non-display

  • きちんと知りたい!飛行機メカニズムの基礎知識

    東野和幸 室蘭工業大学航空宇宙機システム研究センター,日刊協業新聞社,第2章 飛行のための空気力の利用とそのメカニズム(分担)第3章 エンジンによる推進力について(分担),(p.184),2018.01,978-4-526-07785-2

  • Heat Exchanger Basic Design Application

    R. Minato, K. Higashino, M. Sugioka and Y. Sasayama,INTECH,(p.585),2012.03,978-953-51-0278-6

Papers 【 display / non-display

  • Low Toxic Nitromethane Based Monopropellant for Gas Generator Cycle Air Turbo Ramjet Engine

    Ryojiro Minato,Propulsion and Power Research,vol.11,(3),(p.311 ~ 324),2022.09

  • Fluid Hammer Phenomena for Nitromethane Propellant Feed System

    R. Minato, S. Tanaka,Science and Technology of Energetic Materials,vol.83,(4),(p.111 ~ 116),2022.08

  • Study on Propellant Supply System for a Small-scale Supersonic Flight Experiment Vehicle (Study on a Propellant Management Device)

    2. Naoki Sota, Ryoji Imai, Aoki Anada, Taisei Yamazaki, Masaharu Uchiumi, Daisuke Nakata, and Ryojiro Minato,International Journal of Microgravity of Science Application,vol.39,(1),(p.390103 ~ ),2022.01

  • Overspeeding Characteristics of Turbomachinery for Gas Generator Cycle Air Turbo Ramjet Engine

    R. Minato, D. Nakata, M. Uchiumi, R. Imai, K. Higashino,Propulsion and Power Research,2022

  • On the Pressure Loss Characteristics of Liquid Oxygen Considering a Heat Input

    Daisuke Nakata, Ryojiro Minato, Inaho Yoshikawa, Hiromitsu Yagihashi, and Masaharu Uchiumi,Transactions of the Japan Society for Aeronautical and Space Sciences,vol.19,(2),(p.217 ~ 223),2021.03

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International conference proceedings 【 display / non-display

  • Dual Manifold Flow Control System for Gas-Generator Cycle Air Ramjet Engine

    Ryojiro Minato, Daisuke Nakata, Masaharu Uchiumi, Inaho, Yoshikawa, Hiromitsu, Yagihashi and Kouki Arimatsu,24th International Society of Air Breathing Engine,2019.09,Canberra, Australia

  • Hot Gas Temperature Distribution in a Gas-Generator for Air Turbo Ramjet Engine

    Daisuke Nakata, Ryojiro Minato, Hiromitsu Yagihashi, Koki Arimatsu, Inaho Yoshikawa, Satoshi Inazumi, Masaya Sumiyoshi, Masaharu Uchiumi,24th International Society of Air Breathing Engine,2019.09,Canberra, Australia

  • Experimental Study of Temperature and Phase Transition of Liquid Oxygen at Ignition in Impinging Injector of Gas Generator

    Hiromitsu Yagihashi, Daisuke Nakata, Ryojiro Minato, Inaho Yoshikawa, Koki Arimatsu, Masaharu Uchiumi,ASME-JSME-KSME 2019 Joint Fluids Engineering Conference AJKFLUIDS2019,American Society of Mechanical Engineering,2019.07,San Francisco

  • The Minimum Flow Rate of Liquid Oxygen when Considering a Throttling of a Gas Generator Cycle Engineof

    Daisuke Nakata, Ryojiro Minato, Inaho Yoshikawa, Hiromitsu Yagihashi, Koki Arimatsu and Masaharu Uchiumi,ASME-JSME-KSME 2019 Joint Fluids Engineering Conference AJKFLUIDS2019,American Society of Mechanical Engineering,2019.07,San Francisco

  • On the Pressure Loss Characteristics of Liquid Oxygen Considering a Heat Input

    Koki Arimatsu, Daisuke Nakata, Ryojiro Minato, Inaho Yoshikawa, Hiromitsu Yagihashi, Masaharu Uchiumi,32nd International Symposium on Space Technology and Science,The Japan Society of Aeronautical and Space Science,2019.06,福井

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Editorial and Commentary 【 display / non-display

  • 室蘭工業大学航空宇宙機システム研究センター吸込み式超音速風洞の紹介

    東野和幸 高木正平 溝端一秀 湊亮二郎 中田大将 今井良二 棚次亘弘,日本航空宇宙学会誌,vol.63,(6),(p.18 ~ 22),2015.06

Research reports 【 display / non-display

  • 我が国独自の超音速飛行機やスペースプレーン開発のための飛行実験創生事業における空理器実験装置複合体の構築

    溝端一秀、棚次亘弘、杉山弘、新井隆景、湊亮二郎,室蘭工大紀要,vol.54,(p.11 ~ 19),2004

  • Velocity Slip in free jets of gas mixture expanding into a vacuum

    南部健一 湊 亮二郎,東北大学流体科学研究所報告,vol.7,(p.103 ~ 121),1996

Presentaion at conference, meeting, etc. 【 display / non-display

  • ニトロメタン推進剤の水撃作用に関する研究

    湊 亮二郎,田中茂,日本航空宇宙学会北部支部講演会,日本航空宇宙学会,日本航空宇宙学会北部支部講演会講演集,2022.03.18,仙台,Japan

  • GG-ATRエンジン用粒子ダンパー作動特性に関する研究

    湊 亮二郎,佐々木 光、内海 政春,第65回宇宙科学連合講演会,第65回宇宙科学技術連合講演会講演集,2021.11.09,山形,Japan

  • ガスジェネレータサイクル・エアターボラム ジェットエンジン用粒子ダンパーの作動特性 について

    中西 潤、湊 亮二郎、 中田 大将、 内海 政春,日本航空宇宙学会北部支部講演会,日本航空宇宙学会北部支部講演会講演集,2021.03.18

  • 小型超音速飛行実験機向け 推薬供給システム に関する研究(水を用いたガス巻き込み抑制機構の性能検証)

    [529] 曽田直希 ,穴田蒼輝,今井良二,中田大将, 湊亮二郎,内海政春,第18回HASTIC学術技術講演会,第18回HASTIC学術技術講演会講演集,2021.03.03

  • 小型無人超音速飛行実験機における酸化剤タンク内熱流動挙動に関する研究

    [531] 濱田慶一郎,清水 建登,湊 亮二郎,中田大将,内海政春,今井良二,第18回HASTIC学術技術講演会,第18回HASTIC学術技術講演会講演集,2021.03.03

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Patent acquisition 【 display / non-display

  • タービン駆動用ガスジェネレータの推進剤及びその製造方法

    特願2018-179736,特開2020-050721

 

Class subject in charge 【 display / non-display

  • フレッシュマンセミナー(Dクラス)

    2022,Department

  • ロケット工学

    2022,Department

  • 宇宙機設計法

    2022,Department

  • 航空宇宙熱力学

    2022,Department

  • 航空宇宙工学セミナー

    2022,Department

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