Wakita Masashi

ワキタマサシ | Wakita Masashi

Affiliation and department：
Homepage URL (1)： http://kaken.nii.ac.jp/d/r/80451441.ja.html

Research field (1)： Aerospace engineering

Research keywords (9)：燃焼工学 , 熱工学 , 衝撃波 , 航空宇宙工学 , デトネーション , パルスデトネーションエンジン , 超音速燃焼 , ハイブリッドロケット , 燃焼

Research theme for competitive and other funds (12)：

2022 - 2026 液体酸素を用いる端面燃焼式ハイブリッドロケットの実証研究
2020 - 2023 小型宇宙機に革新的軌道変換能力を与えるハイブリッドキックモータの開発
2019 - 2022 Nozzle throat erosion mechanisms in hybrid rockets
2019 - 2022 Elucidation of Diffusion Flame Mechanism of Liquid Oxygen-Solid Fuel and its Application to End-Burning Hybrid Rocket
2019 - 2022 液体酸素-固体燃料の拡散燃焼機構の解明と端面燃焼式ハイブリッドロケットへの適用

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Papers (54)：

Masashi Wakita, Yusuke Takada, Kodai Iwanaga, Toshiaki Iizuka, Hironori Sahara, Landon T. Kamps, Harunori Nagata. Application of Low Concentration Hydrogen Peroxide for Hybrid Rocket Propulsion System for Small Spacecraft. AIAA AVIATION 2022 Forum. 2022
ONO Genta, IWANAGA Kodai, TAKADA Yusuke, WAKITA Masashi, Kamps Landon, NAGATA Harunori. Flame-Holding Characteristics of a Hybrid Rocket using Pre-heated 60wt% Hydrogen Peroxide. The Proceedings of Mechanical Engineering Congress, Japan. 2022. 2022. J191-07
Yusuke Takada, Kodai Iwanaga, Hajime Inoue, Shota Inoue, Masashi Wakita, Landon T. Kamps, Hironori Sahara, Toshiaki Iizuka, Harunori Nagata. Ignition and flame-holding characteristics of 60wt% hydrogen peroxide in a CAMUI-type hybrid rocket fuel. AIAA Propulsion and Energy 2021 Forum. 2021
Ayumu Tsuji, Ai Yamada, Mai Fukada, Landon T. Kamps, Masashi Wakita, Harunori Nagata. Experimental and Numerical Investigation of Throttling Response Mechanisms in Axial-Injection End-Burning Hybrid Rockets. AIAA Propulsion and Energy 2021 Forum. 2021
Ayumu Tsuji, Yuji Saito, Landon Kamps, Masashi Wakita, Harunori Nagata. Stabilized combustion of circular fuel duct with liquid oxygen. Proceedings of the Combustion Institute. 2021. 38. 3. 4845-4855

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MISC (207)：

永田晴紀, 鈴木翔, 李介維, 添田健太郎, KAMPS Landon, 脇田督司. Development of End-burning Hybrid Rocket Using Liquid Oxygen as Oxidizer. 宇宙科学技術連合講演会講演集(CD-ROM). 2022. 66th
野中, 響己, 津地, 歩, 李, 介維, 永田, 晴紀, 脇田, 督司, NONAKA, Hibiki, TSUJI, Ayumu, LI, Kaii, NAGATA, Harunori, WAKITA, Masashi. 液体酸素が流れる固体燃料管列の燃え拡がり特性-Flame Spreading Characteristics of Solid Fuel Tube Row with Liquid Oxygen. 令和3年度宇宙輸送シンポジウム: 講演集録 = Proceedings of Space Transportation Symposium FY2021. 2022
岩永昂大, 高田裕亮, 小野玄太, 脇田督司, KAMPS Landon, 佐原宏典, 飯塚俊明, 永田晴紀. Flame-Holding Characteristics of 60wt% Hydrogen Peroxide Hybrid Rocket with Platinum Catalysts. 燃焼シンポジウム講演論文集(CD-ROM). 2021. 59th
津地歩, 山田藍, 深田真衣, 脇田督司, 永田晴紀. Simulation of Throttling Response in Axial-Injection End-Burning Hybrid Rocket. 日本機械学会年次大会講演論文集(CD-ROM). 2020. 2020
深田真衣, 佐藤元紀, 津地歩, 永田晴紀, 脇田督司. Boundary Condition between Flame Spreading and Stabilized Combustion with Nitrous Oxide and PMMA. 日本機械学会年次大会講演論文集(CD-ROM). 2020. 2020

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Education (3)：

2003 - 2006 Hokkaido University Graduate School of Engineering Division of Mechanical Science
2001 - 2003 Hokkaido University
1997 - 2001 Hokkaido University

Professional career (1)：

博士(工学) (北海道大学)

Work history (3)：

2008/10 - 現在北海道大学工学(系)研究科(研究院) 助教
2007/10 - 2008/09 Kyushu Institute of Technology School of Engineering
2006/08 - 2007/09 Hokkaido University Graduate School of Engineering

Committee career (3)：

2016/02 - 現在第30回宇宙技術および科学の国際シンポジウム組織委員会プログラム小委員会(Chemical Propulsion and Air-breathing Engines)委員
2015 - 現在日本航空宇宙学会宇宙利用部門幹事
2021/04 - 2023/03 日本機械学会宇宙工学部門広報委員会幹事

Association Membership(s) (4)：

The American Institute of Aeronautics and Astronautics , COMBUSTION SOCIETY OF JAPAN , THE JAPAN SOCIETY AERONAUTICAL AND SPACE SCIENCES , THE JAPAN SOCIETY OF MECHANICAL ENGINEERS

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