Wakita Masashi 脇田督司

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WAKITA Masashi 脇田督司

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Researcher Number	80451441
Other IDs
External Links
Affiliation (Current)	2025: 北海道大学, 工学研究院, 助教
Affiliation (based on the past Project Information) *help	2019 – 2024: 北海道大学, 工学研究院, 助教 2016 – 2017: 北海道大学, 工学研究院, 助教 2015: 北海道大学, 大学院工学研究院, 助教 2012 – 2015: 北海道大学, 工学(系)研究科(研究院), 助教 2010 – 2011: 北海道大学, 大学院・工学研究院, 助教 2008 – 2009: Hokkaido University, 大学院・工学研究科, 助教 2007: Kyushu Institute of Technology, 工学部, 博士研究員
Review Section/Research Field	Principal Investigator Aerospace engineering / Basic Section 24010:Aerospace engineering-related / Thermal engineering Except Principal Investigator Aerospace engineering / Medium-sized Section 24:Aerospace engineering, marine and maritime engineering, and related fields / Transformative Research Areas, Section (II) / Basic Section 24010:Aerospace engineering-related
Keywords	Principal Investigator デトネーション / パルスデトネーションエンジン / ドライバーガス過供給 / 水素-空気混合気 / 超音速燃焼 / 液体酸素 / 端面燃焼式ハイブリッドロケット / 3Dプリンタ / 推進 / 拡散火炎 … More / 固体燃焼 / 液体酸化剤 / 端面燃焼 / ハイブリッドロケット / イニシエーション / デトネーションの伝播 / 円錐形状反射板 / 反射板 / 反射板ドライバーガス過供給 … More Except Principal Investigator ハイブリッドロケット / ロケット / 固体燃焼 / ノズル浸食 / 燃焼 / 宇宙推進 / 地上燃焼実験 / 再現法 / 航空宇宙工学 / スケール効果 / 光造形 / 3D印刷 / 端面燃焼 / 端面燃焼式 / 推進 / 宇宙 / 軌道変換 / 小型宇宙機 / キックモータ / 軌道変換ロケット / 小型相乗り宇宙機 / ノズルエロージョン / ノズル侵食 / ロケットノズル / 推進・エンジン / 宇宙輸送 / 宇宙インフラ / 遺伝的アルゴリズム / 衝突噴流熱伝達 Less

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
- Principal Investigator
  
  永田晴紀
- Project Period (FY)
  2022 – 2025
- Research Category
  
  Grant-in-Aid for Scientific Research (A)
- Review Section
  
  Medium-sized Section 24:Aerospace engineering, marine and maritime engineering, and related fields
- Research Institution
  Hokkaido University
Development of a Hybrid Kick Motor to Provide Innovative Orbit-Transfer Capabilities for Micro-Spaceproves
- Principal Investigator
  
  Nagata Harunori
- Project Period (FY)
  2020 – 2022
- Research Category
  
  Grant-in-Aid for Transformative Research Areas (B)
- Review Section
  
  Transformative Research Areas, Section (II)
- Research Institution
  Hokkaido University
Elucidation of Diffusion Flame Mechanism of Liquid Oxygen-Solid Fuel and its Application to End-Burning Hybrid RocketPrincipal Investigator
- Principal Investigator
  
  Wakita Masashi
- Project Period (FY)
  2019 – 2021
- Research Category
  
  Grant-in-Aid for Scientific Research (C)
- Review Section
  
  Basic Section 24010:Aerospace engineering-related
- Research Institution
  Hokkaido University
Nozzle throat erosion mechanisms in hybrid rockets
- Principal Investigator
  
  Nagata Harunori
- Project Period (FY)
  2019 – 2021
- Research Category
  
  Grant-in-Aid for Scientific Research (B)
- Review Section
  
  Basic Section 24010:Aerospace engineering-related
- Research Institution
  Hokkaido University
Method for Determining Nozzle-Throat-Erosion History in Hybrid Rockets and Elucidation of the Mechanism
- Principal Investigator
  
  Nagata Harunori
- Project Period (FY)
  2015 – 2017
- Research Category
  
  Grant-in-Aid for Scientific Research (B)
- Research Field
  
  Aerospace engineering
- Research Institution
  Hokkaido University
Development of Large Diameter Detonation Wave Initiator Using Cylindrical Detonation WavePrincipal Investigator
- Principal Investigator
  
  WAKITA Masashi
- Project Period (FY)
  2013 – 2014
- Research Category
  
  Grant-in-Aid for Young Scientists (B)
- Research Field
  
  Thermal engineering
- Research Institution
  Hokkaido University
Fuel Regression Characteristics of CAMUI-type hybrid rockets under high Reynolds numbers
- Principal Investigator
  
  Nagata Harunori
- Project Period (FY)
  2012 – 2015
- Research Category
  
  Grant-in-Aid for Scientific Research (A)
- Research Field
  
  Aerospace engineering
- Research Institution
  Hokkaido University
Optimal Design Method of CAMUI-type Fuel Grain
- Principal Investigator
  
  NAGATA Harunori
- Project Period (FY)
  2009 – 2011
- Research Category
  
  Grant-in-Aid for Scientific Research (B)
- Research Field
  
  Aerospace engineering
- Research Institution
  Hokkaido University
Development of Pulse Detonation Engine Initiator Using Conic Shape Reflector for Large Bore and High thrust CombustorPrincipal Investigator
- Principal Investigator
  
  WAKITA Masashi
- Project Period (FY)
  2009 – 2011
- Research Category
  
  Grant-in-Aid for Young Scientists (B)
- Research Field
  
  Aerospace engineering
- Research Institution
  Hokkaido University
Research on detonation initiation mechanism with reflecting boardfor pulse detonation enginePrincipal Investigator
- Principal Investigator
  
  WAKITA Masashi
- Project Period (FY)
  2007 – 2008
- Research Category
  
  Grant-in-Aid for Young Scientists (Start-up)
- Research Field
  
  Aerospace engineering
- Research Institution
  Hokkaido University
  Kyushu Institute of Technology

[Journal Article] Ignition and flame-holding characteristics of 60wt% hydrogen peroxide in a CAMUI-type hybrid rocket fuel2021
- Author(s)
  Takada Yusuke、Iwanaga Kodai、Inoue Hajime、Inoue Shota、Wakita Masashi、Kamps Landon T.、Sahara Hironori、Iizuka Toshiaki、Nagata Harunori
- Journal Title
  
  AIAA Propulsion and Energy Forum
  
  Volume: - Pages: 0-0
- DOI
  10.2514/6.2021-3511
- Peer Reviewed
- Data Source
  KAKENHI-PLANNED-20H05747, KAKENHI-PROJECT-19H02336
[Journal Article] Stabilized combustion of circular fuel duct with liquid oxygen2020
- Author(s)
  Tsuji Ayumu、Saito Yuji、Kamps Landon、Wakita Masashi、Nagata Harunori
- Journal Title
  
  Proceedings of the Combustion Institute
  
  Volume: 38 Issue: 3 Pages: 4845-4855
- DOI
  10.1016/j.proci.2020.07.001
- Peer Reviewed
- Data Source
  KAKENHI-PROJECT-19K04832
[Journal Article] Method for Determining Nozzle-Throat-Erosion History in Hybrid Rockets2017
- Author(s)
  Kamps, L., Saito, Y., Kawabata, R., Wakita, M., Totani, T., Takahashi, Y., and Nagata, H
- Journal Title
  
  Journal of Propulsion and Power
  
  Volume: 33 Issue: 6 Pages: 1369-1377
- DOI
  10.2514/1.b36390
- NAID
  120006366503
- Peer Reviewed / Open Access
- Data Source
  KAKENHI-PROJECT-15H04197
[Journal Article] Estimation of Hybrid Rocket Nozzle Throat Erosion History2016
- Author(s)
  Yuji SAITO, Tsutomu UEMATSU, Hikaru ISOCHI, Masashi WAKITA, Tsuyoshi TOTANI, Harunori NAGATA
- Journal Title
  
  AEROSPACE TECHNOLOGY JAPAN
  
  Volume: 14 Issue: ists30 Pages: Pa_145-Pa_151
- DOI
  10.2322/tastj.14.Pa_145
- NAID
  130005331202
- ISSN
  1884-0485
- Language
  English
- Peer Reviewed / Acknowledgement Compliant
- Data Source
  KAKENHI-PROJECT-15H04197
[Journal Article] Effect of Combustion Pressure on Regression Rate of Solid Fuel under an Impinging Oxidizer Jet Counterflow Diffusion Flame2014
- Author(s)
  Ken Terakawa, Tatsuya Saito, Yuji Nakamura, Tsuneyoshi Matsuoka, Harunori Nagata, Tsuyoshi Totani, Masashi Wakita
- Journal Title
  
  Journal of Thermal Science and Technology
  
  Volume: 9
- NAID
  130004678606
- Peer Reviewed / Acknowledgement Compliant
- Data Source
  KAKENHI-PROJECT-24246135
[Journal Article] Influence of detonation cell size on propagation of cylindrical detonation wave2014
- Author(s)
  Masashi WAKITA, Kazuya SAJIKI, Tsunetaro HIMONO, Tsuyoshi TOTANI and Harunori NAGATA
- Journal Title
  
  TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
  
  Volume: 12
- NAID
  130003395428
- Peer Reviewed
- Data Source
  KAKENHI-PROJECT-25870006
[Journal Article] Accuracy and applicable range of a reconstruction technique for hybrid rockets2014
- Author(s)
  Harunori Nagata, Hisahiro Nakayama, Mikio Watanabe, Masashi Wakita and Tsuyoshi Totani
- Journal Title
  
  Advances in Aircraft and Spacecraft Science
  
  Volume: 1 Issue: 3 Pages: 273-289
- DOI
  10.12989/aas.2014.1.3.273
- Peer Reviewed / Acknowledgement Compliant / Open Access
- Data Source
  KAKENHI-PROJECT-24246135
[Journal Article] Development and Flight Demonstration of 5 kN Thrust Class CAMUI Type Hybrid Rocket2014
- Author(s)
  Harunori NAGATA, Masashi WAKITA, Tsuyoshi TOTANI, Tsutomu UEMATSU
- Journal Title
  
  AEROSPACE TECHNOLOGY JAPAN
  
  Volume: 12 Issue: ists29 Pages: Ta_1-Ta_4
- DOI
  10.2322/tastj.12.Ta_1
- NAID
  130003395437
- ISSN
  1884-0485
- Language
  English
- Peer Reviewed / Acknowledgement Compliant / Open Access
- Data Source
  KAKENHI-PROJECT-24246135
[Journal Article] Development of Pulse Detonation Engine Initiator Using Reflector for Large Bore Combustor2012
- Author(s)
  Masashi Wakita
- Journal Title
  
  AEROSPACE TECHNOLOGY JAPAN
  
  Volume: 10 Issue: ists28 Pages: Pa_31-Pa_36
- DOI
  10.2322/tastj.10.Pa_31
- NAID
  130002137028
- ISSN
  1884-0485
- Language
  English
- Peer Reviewed
- Data Source
  KAKENHI-PROJECT-21760646
[Journal Article] Development of Pulse Detonation Engine Initiator Using Reflector for Large Bore Combustor2012
- Author(s)
  Masashi WAKITA, Masayoshi TAMURA, Akihiro TERASAKA, Kazuya SAJIKI, Tsuyoshi TOTANI and Harunori NAGATA
- Journal Title
  
  TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
  
  Volume: Vol.10, No.ists28 Pages: 31-36
- NAID
  130002137028
- Data Source
  KAKENHI-PROJECT-21760646
[Journal Article] Driver Gas Reduction Effect of Pulse-Detonation-Engine Initiator Using Reflecting Board2011
- Author(s)
  Masashi Wakita, Ryusuke Numakura, Takatoshi Asada, Masayoshi Tamura, Tsuyoshi Totani and Harunori Nagata
- Journal Title
  
  Journal of Propulsion and Power
  
  Volume: Vol.27, No.1 Pages: 162-170
- Data Source
  KAKENHI-PROJECT-21760646
[Journal Article] Driver Gas Reduction Effect of Pulse-Detonation-Engine Initiator Using Reflecting Boar2011
- Author(s)
  Masashi Wakita
- Journal Title
  
  JOURNAL OF PROPULSION AND POWER
  
  Volume: 27 Pages: 162-170
- Peer Reviewed
- Data Source
  KAKENHI-PROJECT-21760646
[Journal Article]2010
- Author(s)
  Y. Kaneko, K. Kishida, N. Oshima, T. Nakashima, M. Wakita, T. Totani, H. Nagata
- Journal Title
  
  Journal of Space Engineering
  
  Volume: Vol.3, No.1 Pages: 52-65
- Peer Reviewed
- Data Source
  KAKENHI-PROJECT-21360410
[Journal Article] Preliminary Design of Winged Experimental Rocket by University Consortium2009
- Author(s)
  M.Wakita, 他5名
- Journal Title
  
  Transactions of the Japan Society for Aeronautical and Space Sciences, Space Technology Japan 7
- NAID
  130000151877
- Peer Reviewed
- Data Source
  KAKENHI-PROJECT-21360410
[Journal Article] Transactions of the Japanese Society for Aeronautical and Space Sciences2009
- Author(s)
  Y. Kaneko, M. Itoh, A. Kakikura, K. Mori, K. Uejima, T. Nakashima, M. Wakita, T. Totani, N. Oshima, H. Nagata
- Journal Title
  
  Space Technology Japan
  
  Volume: Vol.7, No.ists26
- Peer Reviewed
- Data Source
  KAKENHI-PROJECT-21360410
[Presentation] Combustion Characteristics of Stabilized Combustion with Liquid Oxygen at Different Operating Conditions2024
- Author(s)
  Suzuki, S., Son, T., Lyons, K., Minami, K., Fukada, M., Maebayashi, H., Gallo, G., Wakita, M., and Nagata, H.
- Organizer
  AIAA SCITECH 2024 Forum
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-22H00240
[Presentation] Application of Low Concentration Hydrogen Peroxide for Hybrid Rocket Propulsion System for Small Spacecraft2023
- Author(s)
  Masashi Wakita, Yusuke Takada, Kodai Iwanaga, Toshiaki Iizuka, Hironori Sahara, Landon T. Kamps and Harunori Nagata
- Organizer
  AIAA SCITECH 2023 Forum
- Int'l Joint Research
- Data Source
  KAKENHI-PLANNED-20H05747
[Presentation] Combustion Characteristics of Axial-Injection End-Burning Hybrid Rockets using Liquid Oxygen2023
- Author(s)
  Suzuki, S., Minami, K., Son, s., Fukada, M., Kamps, L., Wakita, M., and Nagata, H.
- Organizer
  74th International Astronautical Congress
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-22H00240
[Presentation] Fuel regression characteristics of axial-injection end-burning hybrid rockets using Nitrous Oxide2022
- Author(s)
  Mai Fukada, Hiroki Hayasaka, Sho Suzuki, Landon Kamps, Masashi Wakita, Harunori Nagata
- Organizer
  73rd International Astronautical Congress 2022
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-22H00240
[Presentation] 液体酸素を用いる端面燃焼式ハイブリッドロケット実機開発にむけた基盤データ構築2022
- Author(s)
  李介維，野中響己，鈴木翔，深田真衣，ケンプスランドン，脇田督司，永田晴紀
- Organizer
  日本機械学会北海道学生会第51回学生員卒業研究発表講演会
- Data Source
  KAKENHI-PROJECT-19K04832
[Presentation] 液体酸素が流れる固体燃料管列の燃え拡がり特性2022
- Author(s)
  野中響己、津地歩、李介維、永田晴紀、脇田督司
- Organizer
  令和3年度宇宙輸送シンポジウム
- Data Source
  KAKENHI-PROJECT-19K04832
[Presentation] Stabilized Combustion of Circular Fuel Duct with Liquid Oxygen2020
- Author(s)
  Ayumu Tsuji, Yuji Saito, Landon Kamps, Masashi Wakita, Harunori Nagata
- Organizer
  38th International Symposium on Combustion
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-19K04832
[Presentation] 端面燃焼式ハイブリッドロケットの推力制御応答に関するシミュレーション2020
- Author(s)
  津地歩, 深田真衣, 山田藍, 脇田督司, 永田晴紀
- Organizer
  2020年度日本機械学会年次大会
- Data Source
  KAKENHI-PROJECT-19K04832
[Presentation] Stabilized Combustion of Circular Fuel Duct with Liquid Oxygen2020
- Author(s)
  Ayumu Tsuji, Yuji Saito, Kamps Landon, Masashi Wakita, Harunori Nagata,
- Organizer
  38th International Symposium on Combustion
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-19K04832
[Presentation] ハイブリッドロケットの軸方向後燃料退速度に関する３Dスキャナを用いた研究2020
- Author(s)
  奥田晃崇，Landon Kamps，伊藤聖司，影山理沙，Tor Viscor，井上翔太，池田華子，高田祐亮，脇田督司，永田晴紀
- Organizer
  第58回燃焼シンポジウム
- Data Source
  KAKENHI-PLANNED-20H05747
[Presentation] 液体酸素供給端面燃焼式ハイブリッドロケットの設計と実現可能性検討2019
- Author(s)
  津地歩, 脇田督司, 永田晴紀
- Organizer
  第2回ハイブリッドロケットシンポジウム
- Data Source
  KAKENHI-PROJECT-19K04832
[Presentation] アブレータ材料によるハイブリッドロケットノズル浸食抑制に関する研究2019
- Author(s)
  奥田晃崇,Landon T. Kamps,櫻井和人, 井上卓,Tor Viscor,内山絵里香,池田華子, 吉丸利,脇田督司,永田晴紀
- Organizer
  第57回燃焼シンポジウム
- Data Source
  KAKENHI-PROJECT-19H02336
[Presentation] 超小型深宇宙探査機用ハイブリッドキックモータの開発2019
- Author(s)
  伊藤聖司,Kamps Landon,櫻井和人,内山絵里香,影山理沙,脇田督司,永田晴紀
- Organizer
  日本機械学会 2019年度年次大会
- Data Source
  KAKENHI-PROJECT-19H02336
[Presentation] ハイブリッドロケットにおけるノズルスロートエロージョン抑制材料に関する研究2016
- Author(s)
  山口亮、川端良輔、平井翔大、ケンプスランドン、脇田督司、戸谷剛、永田晴紀
- Organizer
  日本機械学会 2016年度年次大会
- Place of Presentation
  九州大学伊都キャンパス（福岡市）
- Year and Date
  2016-09-11
- Data Source
  KAKENHI-PROJECT-15H04197
[Presentation] Estimation of Hybrid Rocket Nozzle Throat Erosion History2015
- Author(s)
  Yuji SAITO, Tsutomu UEMATSU, Hikaru ISOCHI, Masashi WAKITA, Tsuyoshi TOTANI Harunori NAGATA
- Organizer
  30th International Symposium on Space Technology and Science
- Place of Presentation
  Tokyo
- Year and Date
  2015-07-10
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-15H04197
[Presentation] Nozzle Erosion Progress in Hybrid Rocket Firings2015
- Author(s)
  Ryosuke Kawabata, Yuji Saito, Shota Hirai, Barnier Camille, Masashi Wakita, Tsuyoshi Totani, Harunori Nagata,
- Organizer
  Twelfth International Conference on Flow Dynamics
- Place of Presentation
  Sendai, Japan
- Year and Date
  2015-10-28
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-15H04197
[Presentation] ハイブリッドロケットのノズル侵食履歴およびノズルスロート温度履歴の取得2015
- Author(s)
  永田晴紀、川端良輔、遠藤瞳、金井竜一郎、平井翔大、脇田督司、戸谷剛、五十地輝
- Organizer
  第53回燃焼シンポジウム
- Place of Presentation
  つくば国際会議場
- Year and Date
  2015-11-17
- Data Source
  KAKENHI-PROJECT-15H04197
[Presentation] ハイブリッドロケットにおけるノズルスロートエロージョンに関する研究2015
- Author(s)
  川端良輔, 齋藤勇士, 平井翔大, 脇田督司, 戸谷剛, 永田晴紀
- Organizer
  第59回宇宙科学技術連合講演会
- Place of Presentation
  かごしま県民交流センター
- Year and Date
  2015-10-07
- Data Source
  KAKENHI-PROJECT-15H04197
[Presentation] 低レイノルズ数域におけるCAMUI型固体燃料の燃料後退特性2014
- Author(s)
  遠藤瞳、川端良輔、脇田督司、戸谷剛、永田晴紀
- Organizer
  第52回燃焼シンポジウム
- Place of Presentation
  岡山コンベンションセンター
- Year and Date
  2014-12-05
- Data Source
  KAKENHI-PROJECT-24246135
[Presentation] ハイブリッドロケット燃焼データ解析法の精度と適用範囲に関する研究2014
- Author(s)
  齋藤勇士、Aurelien Lambourg、川端良輔、脇田督司、戸谷剛、永田晴紀
- Organizer
  宇宙科学技術連合講演会
- Place of Presentation
  長崎ブリックホール
- Year and Date
  2014-11-13
- Data Source
  KAKENHI-PROJECT-24246135
[Presentation] 酸化剤衝突噴流による固体燃料燃焼場の数値解析2014
- Author(s)
  縄田和也、大島伸行、斉藤達也、脇田督司、戸谷剛、永田晴紀
- Organizer
  宇宙科学技術連合講演会
- Place of Presentation
  長崎ブリックホール
- Year and Date
  2014-11-13
- Data Source
  KAKENHI-PROJECT-24246135
[Presentation] 一定レイノルズ数酸化剤衝突噴流のよどみ点近傍における固体燃料燃焼速度に雰囲気圧力が及ぼす影響2014
- Author(s)
  斉藤竜也、寺川健、脇田督司、戸谷剛、永田晴紀
- Organizer
  第52回燃焼シンポジウム
- Place of Presentation
  岡山コンベンションセンター
- Year and Date
  2014-12-05
- Data Source
  KAKENHI-PROJECT-24246135
[Presentation] 推力15kN級CAMUI型ハイブリッドロケットモーターの開発2014
- Author(s)
  川端良輔、永田晴紀、戸谷剛、脇田督司、五十地輝、植松努
- Organizer
  宇宙科学技術連合講演会
- Place of Presentation
  長崎ブリックホール
- Year and Date
  2014-11-13
- Data Source
  KAKENHI-PROJECT-24246135
[Presentation] 円筒波の起爆と希釈燃料への伝播に流路幅が与える影響2014
- Author(s)
  桧物恒太郎, 菊地敬太, 亀山頌太，脇田督司, 戸谷剛, 永田晴紀
- Organizer
  平成25年度衝撃波シンポジウム
- Place of Presentation
  神奈川県相模原市　青山学院大学相模原キャンパス
- Data Source
  KAKENHI-PROJECT-25870006
[Presentation] 上空打ち上げ用ハイブリッドロケットのための断熱液体酸素タンクの検討2014
- Author(s)
  川端良輔、稲場康彦、石山達也、脇田督司、戸谷剛、永田晴紀
- Organizer
  日本機械学会年次大会
- Place of Presentation
  東京電機大学
- Year and Date
  2014-09-07
- Data Source
  KAKENHI-PROJECT-24246135
[Presentation] 円盤状流路に入射する平面デトネーション波の半径方向に伝播する円筒波への遷移にプリデトネータ直径が与える影響2013
- Author(s)
  桧物恒太郎, 菊地敬太，脇田督司, 戸谷剛, 永田晴紀
- Organizer
  第51回燃焼シンポジウム
- Place of Presentation
  東京都大田区産業プラザPio
- Data Source
  KAKENHI-PROJECT-25870006
[Presentation] Effects of diluent gas on toroidal detonation wave propagation through gradual expanding channel2013
- Author(s)
  Masashi Wakita, Kazuya Sajiki, Tsunetaro Himono, Tsuyoshi Totani and Harunori Nagata
- Organizer
  24th International Colloquium on Dynamics of Explosion and Reactive Systems
- Place of Presentation
  Taipei, Taiwan, NTUH International Convention Center
- Data Source
  KAKENHI-PROJECT-25870006
[Presentation] Influence of detonation cell size on propagation of cylindrical detonation wave2013
- Author(s)
  Masashi Wakita, Kazuya Sajiki, Tsunetaro Himono, Tsuyoshi Totani and Harunori Nagata
- Organizer
  29th International Symposium on Space Technology and Science
- Place of Presentation
  愛知県名古屋市名古屋国際会議場
- Data Source
  KAKENHI-PROJECT-25870006
[Presentation] CAMUI型固体燃料前端面燃料後退速度式にレイノルズ数および流路形状の与える影響」2012
- Author(s)
  金井竜一朗,石山達也,出雲弘一,野原正寛脇田督司,戸谷剛,永田晴紀
- Organizer
  平成23年度宇宙輸送シンポジウム講演論文集
- Place of Presentation
  STCP
- Data Source
  KAKENHI-PROJECT-21360410
[Presentation] Effect of Reynolds Number on Regression Characteristics around Jet Stagnation Region2011
- Author(s)
  H. Nagata, S. Hagiwara, M. Nohara, M. Wakita, T. Totani
- Organizer
  Proceedings of Eighth International Conference on Flow Dynamics
- Place of Presentation
  Sendai
- Data Source
  KAKENHI-PROJECT-21360410
[Presentation] Development of Pulse Detonation Engine Initiator using Reflector for Large Bore Combustor2011
- Author(s)
  Masashi Wakita, Masayosi Tamura, Akihiro Terasaka, Kazuya Sajiki, Tsuyoshi Totani and Harunori Nagata
- Organizer
  Proc. 28th International Symposium on Space Technology and Science(ISTS)
- Place of Presentation
  Naha, Japan
- Data Source
  KAKENHI-PROJECT-21760646
[Presentation] Planar toroidal detonation propagation through gradual expanding channel2011
- Author(s)
  Masashi Wakita
- Organizer
  23rd International Colloquium on Dynamics of Explosion and Reactive Systems (23rd ICDERS)
- Place of Presentation
  カリフォルニア大学アーバイン校,(アーバイン,米国)
- Year and Date
  2011-07-18
- Data Source
  KAKENHI-PROJECT-21760646
[Presentation] Development effort of pulse detonation engine initiator using reflector at Hokkaido university2011
- Author(s)
  Masashi Wakita
- Organizer
  International Workshop on Detonation for Propulsion 2011
- Place of Presentation
  Paradise Hotel, Busan, Korea
- Data Source
  KAKENHI-PROJECT-21760646
[Presentation] Development of Pulse Detonation Engine Initiator using Reflector for Large Bore Combustor2011
- Author(s)
  Masashi Wakita
- Organizer
  28th International Symposium on Space Technology and Science (ISTS)
- Place of Presentation
  沖縄コンベンションセンター,(宜野湾市)
- Year and Date
  2011-06-11
- Data Source
  KAKENHI-PROJECT-21760646
[Presentation] Optimal Fuel Grain Design Method for CAMUI Type Hybrid Rocket2011
- Author(s)
  H. Nagata , S. Hagiwara, M. Nohara, M. Wakita, T. Totani
- Organizer
  47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, San Diego
- Place of Presentation
  CL
- Data Source
  KAKENHI-PROJECT-21360410
[Presentation] CAMUI型固体燃料後退速度式の導出方法に関する検討2011
- Author(s)
  野原正寛,萩原俊輔,金子雄大,出雲弘一,脇田督司,戸谷剛,永田晴紀
- Organizer
  2011年度年次大会
- Data Source
  KAKENHI-PROJECT-21360410
[Presentation] 酸化剤噴流淀み点近傍におけるポリエチレン燃料の後退特性2011
- Author(s)
  永田晴紀,金子雄大,脇田督司,戸谷剛
- Organizer
  第49回燃焼シンポジウム講演論文集
- Data Source
  KAKENHI-PROJECT-21360410
[Presentation] CAMUI型ハイブリッドロケットの燃料後退特性に及ぼすレイノルズ数の影響2011
- Author(s)
  永田晴紀,萩原俊輔,野原正寛,脇田督司,戸谷剛,植松努
- Organizer
  平成22年度宇宙輸送シンポジウム講演論文集
- Data Source
  KAKENHI-PROJECT-21360410
[Presentation] Development effort of pulse detonation engine initiator using reflector at Hokkaido university2011
- Author(s)
  Masashi Wakita
- Organizer
  International Workshop on Detonation for Propulsion 2011
- Place of Presentation
  パラダイスホテル,(釜山,韓国)(招待講演)
- Year and Date
  2011-11-15
- Data Source
  KAKENHI-PROJECT-21760646
[Presentation] Planar toroidal detonation propagation through gradual expanding channel2011
- Author(s)
  Masashi Wakita, Masayoshi Tamura, Akihiro Terasaka, Kazuya Sajiki, Tsuyoshi Totani and Harunori Nagata
- Organizer
  Proc. 23rd International Colloquium on Dynamics of Explosion and Reactive Systems(23rd ICDERS)
- Place of Presentation
  Irvine, USA
- Data Source
  KAKENHI-PROJECT-21760646
[Presentation] Development of Regression Formulas for CAMUI Type Hybrid Rockets as Functions of Local O/F2010
- Author(s)
  H. Nagata, S. Hagiwara, Y. Kaneko, M. Wakita, T. Totani, T. Uematsu
- Organizer
  46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
- Place of Presentation
  Nashville, TN
- Data Source
  KAKENHI-PROJECT-21360410
[Presentation] Development of 2500 N Class CAMUI Type Hybrid Rocket for Winged Flight Experiments2010
- Author(s)
  H. Nagata , M. Wakita, T. Totani, T. Uematsu, K. Yonemoto
- Organizer
  61st International Astronautical Congress
- Data Source
  KAKENHI-PROJECT-21360410
[Presentation] 小型有翼ロケット実験機用2500N級CAMUI型ハイブリッドロケットの開発2010
- Author(s)
  永田晴紀,脇田督司,戸谷剛,植松努,米本浩一
- Organizer
  平成21年度宇宙輸送シンポジウム講演論文集
- Data Source
  KAKENHI-PROJECT-21360410
[Presentation] Effects of flow passage shape around reflector on detonetion transition2010
- Author(s)
  Masashi Wakita, Masayoshi Tamura, Akihiro Terasaka, Tsuyoshi Totani and Harunori Nagata
- Organizer
  Proc. 8th International Sympoium on Hazards, Prevention, and Mitigation of Industrial Explosions(8th ISHPMIE)
- Place of Presentation
  Yokohama, Japan
- Data Source
  KAKENHI-PROJECT-21760646
[Presentation] CAMUI型固体燃料の燃料後退予測式取得方法に関する検討2010
- Author(s)
  萩原俊輔,金子雄大,野原正寛,永田晴紀,戸谷剛,脇田督司
- Organizer
  日本機械学会2010年度年次大会講演論文集
- Data Source
  KAKENHI-PROJECT-21360410
[Presentation] Effects of flow passage shape around reflector on detonation transition2010
- Author(s)
  Masashi Wakita
- Organizer
  Eighth International Symposium on Hazards, Prevention, and Mitigation of Industrial Explosions
- Place of Presentation
  慶應義塾大学日吉キャンパス横浜
- Year and Date
  2010-09-07
- Data Source
  KAKENHI-PROJECT-21760646
[Presentation] CAMUI型ハイブリッドロケット燃料の後退速度に及ぼす圧力の影響2010
- Author(s)
  永田晴紀,金子雄大,萩原俊輔,伊藤光紀,脇田督司,戸谷剛
- Organizer
  第54回宇宙科学技術連合講演会
- Data Source
  KAKENHI-PROJECT-21360410
[Presentation] Development of 5000 N Thrust Class CAMUI Type Hybrid Rocket2010
- Author(s)
  H. Nagata, M. Wakita, T. Totani, T. Uematsu
- Organizer
  Proceedings of Sixth International Conference on Flow Dynamics
- Place of Presentation
  Sendai
- Data Source
  KAKENHI-PROJECT-21360410
[Presentation] 小型CAMUI式ハイブリッドロケットの開発と運用2010
- Author(s)
  竹腰卓博,佐藤峻哉,田村正佳,萩原俊輔,松岡常吉,脇田督司,戸谷剛,永田晴紀,植松努
- Organizer
  日本機械学会2010年度年次大会講演論文集
- Data Source
  KAKENHI-PROJECT-21360410
[Presentation] 円錐形状反射板を用いたPDEイニシエータによるドライバーガス削減2009
- Author(s)
  脇田督司, 浅田隆利, 戸谷剛, 永田晴紀
- Organizer
  平成20年度衝撃波シンポジウム講演論文集
- Place of Presentation
  名古屋大学(名古屋)
- Year and Date
  2009-03-18
- Data Source
  KAKENHI-PROJECT-19860002
[Presentation] ライデンフロスト温度以下に冷却された固体燃料の燃焼特性2009
- Author(s)
  飯島直純,金子雄大,脇田督司,戸谷剛,永田晴紀
- Organizer
  第47回燃焼シンポジウム講演論文集
- Data Source
  KAKENHI-PROJECT-21360410
[Presentation] 円錐形状反射板を用いたPDEイニシエータによるドライバーガス削減2009
- Author(s)
  脇田督司
- Organizer
  平成20年度衝撃波シンポジウム
- Place of Presentation
  名古屋大学(名古屋)
- Year and Date
  2009-03-18
- Data Source
  KAKENHI-PROJECT-19860002
[Presentation] PDE燃焼器内の円環流路部を通過するデトネーション波の伝播挙動2009
- Author(s)
  脇田督司
- Organizer
  第53回宇宙科学技術連合講演会
- Place of Presentation
  京都大学吉田南構内(京都)
- Year and Date
  2009-09-10
- Data Source
  KAKENHI-PROJECT-21760646
[Presentation] Effect of Local O/F on Regression Rate of Solid Fuels in CAMUI Hybrid Rocket Motor2009
- Author(s)
  H. Nagata, K. Uejima, S. Hagiwara, M. Wakita, T. Totani, T. Uematsu
- Organizer
  Proceedings of Sixth International Conference on Flow Dynamics
- Place of Presentation
  Sendai
- Data Source
  KAKENHI-PROJECT-21360410
[Presentation] 反射板を用いたPDEイニシエーターにおける反射板径の最適化に関する研究2008
- Author(s)
  浅田隆利, 脇田督司, 戸谷剛, 永田晴紀
- Organizer
  第47回日本機械学会北海道支部講演会講演概要集
- Place of Presentation
  釧路工業高等学校(釧路市)
- Year and Date
  2008-09-27
- Data Source
  KAKENHI-PROJECT-19860002
[Presentation] 反射板を用いたPDEイニシエーターにおけるドライバーガス削減に関する研究2008
- Author(s)
  浅田隆利, 脇田督司, 沼倉龍介, 戸谷剛, 永田晴紀
- Organizer
  平成19年度衝撃波シンポジウム講演論文集
- Place of Presentation
  東京工業大学(東京)
- Year and Date
  2008-03-17
- Data Source
  KAKENHI-PROJECT-19860002
[Presentation] Influence of Channel Width on Propagation of Cylindrical Detonation Wave
- Author(s)
  Shota KAMEYAMA, Shun NAWATA, Tsunetaro HIMONO, Keita KIKUCHI, Masashi WAKITA, Tsuyoshi TOTANI and Harunori NAGATA
- Organizer
  30th International Symposium on Space Technology and Science
- Place of Presentation
  兵庫県神戸市神戸コンベンションセンター
- Year and Date
  2015-07-04 – 2015-07-10
- Data Source
  KAKENHI-PROJECT-25870006
[Presentation] 反射体を用いたPDEイニシエータの円錐部の短縮が爆轟波の伝播に与える影響
- Author(s)
  1)菊地敬太, 亀山頌太, 桧物恒太郎, 脇田督司, 戸谷剛, 永田晴紀
- Organizer
  第52回燃焼シンポジウム
- Place of Presentation
  岡山県岡山市岡山コンベンションセンター
- Year and Date
  2014-12-03 – 2014-12-05
- Data Source
  KAKENHI-PROJECT-25870006
[Presentation] 反射を利用した爆轟波生成装置の連続運転条件における円筒爆轟波の生成
- Author(s)
  2)亀山頌太, 菊地敬太, 桧物恒太郎, 脇田督司, 戸谷剛, 永田晴紀
- Organizer
  第46回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム
- Place of Presentation
  青森県弘前市弘前文化センター
- Year and Date
  2014-07-03 – 2014-07-04
- Data Source
  KAKENHI-PROJECT-25870006
[Presentation] RECENT PROGRESS ON DEVELOPMENT OF PULSE DETONATION ENGINE INITIATOR USING REFLECTOR IN HOKKAIDO UNIVERSITY
- Author(s)
  Masashi Wakita
- Organizer
  2014 International Workshop on Detonation for Propulsion (2014 IWDP)
- Place of Presentation
  Institute of Aviation , Warsaw, Poland
- Year and Date
  2014-06-22 – 2014-06-24
- Invited
- Data Source
  KAKENHI-PROJECT-25870006
[Presentation] 反射板を有する円管状燃焼器におけるデトネーション遷移過程の研究
- Author(s)
  浅田隆利, 脇田督司, 戸谷剛, 永田晴紀, 坪井伸幸, 林光一
- Organizer
  平成20年度衝撃波シンポジウム講演論文集
- Place of Presentation
  名古屋大学(名古屋)
- Data Source
  KAKENHI-PROJECT-19860002

1. NAGATA Harunori (40281787)

# of Collaborated Projects: 7 results

# of Collaborated Products: 46 results
2. TOTANI Tsuyoshi (00301937)

# of Collaborated Projects: 3 results

# of Collaborated Products: 31 results
3. 添田建太郎 (30795050)

# of Collaborated Projects: 2 results

# of Collaborated Products: 0 results
4. KAMPS LANDON (70869502)

# of Collaborated Projects: 2 results

# of Collaborated Products: 5 results
5. OSHIMA NOBUYUKI (10217135)

# of Collaborated Projects: 1 results

# of Collaborated Products: 0 results
6. 谷口伸行

# of Collaborated Projects: 0 results

# of Collaborated Products: 1 results

Wakita Masashi 脇田 督司

WAKITA Masashi 脇田 督司

Research Projects

Research Products

Co-Researchers

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

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Development of a Hybrid Kick Motor to Provide Innovative Orbit-Transfer Capabilities for Micro-Spaceproves

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Elucidation of Diffusion Flame Mechanism of Liquid Oxygen-Solid Fuel and its Application to End-Burning Hybrid RocketPrincipal Investigator

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Nozzle throat erosion mechanisms in hybrid rockets

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Method for Determining Nozzle-Throat-Erosion History in Hybrid Rockets and Elucidation of the Mechanism

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Development of Large Diameter Detonation Wave Initiator Using Cylindrical Detonation WavePrincipal Investigator

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Fuel Regression Characteristics of CAMUI-type hybrid rockets under high Reynolds numbers

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Optimal Design Method of CAMUI-type Fuel Grain

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Development of Pulse Detonation Engine Initiator Using Conic Shape Reflector for Large Bore and High thrust CombustorPrincipal Investigator

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Research on detonation initiation mechanism with reflecting boardfor pulse detonation enginePrincipal Investigator

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[Journal Article] Ignition and flame-holding characteristics of 60wt% hydrogen peroxide in a CAMUI-type hybrid rocket fuel2021

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[Journal Article] Stabilized combustion of circular fuel duct with liquid oxygen2020

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[Journal Article] Method for Determining Nozzle-Throat-Erosion History in Hybrid Rockets2017

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DOI

NAID

Wakita Masashi 脇田督司

WAKITA Masashi 脇田督司