Soeda Kentarou 添田建太郎

… Alternative Names

SOEDA KENTARO 添田建太郎

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Researcher Number	30795050
Affiliation (Current)	2025: 東京大学, 大学院理学系研究科(理学部), 特任研究員
Affiliation (based on the past Project Information) *help	2017 – 2024: 東京大学, 大学院理学系研究科(理学部), 特任研究員
Review Section/Research Field	Principal Investigator Aerospace engineering Except Principal Investigator Medium-sized Section 24:Aerospace engineering, marine and maritime engineering, and related fields / Basic Section 24010:Aerospace engineering-related
Keywords	Principal Investigator エンジン / 推進 / 拡散火炎 / 応答特性 / 消炎距離 / 燃焼応答特性 / 光造形 / 端面燃焼 / ハイブリッドロケット Except Principal Investigator 固体燃焼 … More / 端面燃焼 / ハイブリッドロケット / 光造形 / 3D印刷 / ロケット / 宇宙推進 / 端面燃焼式 / 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 / 液体酸化剤 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
Elucidation of Diffusion Flame Mechanism of Liquid Oxygen-Solid Fuel and its Application to End-Burning Hybrid Rocket
- 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
Practical use study of the Axial-Injection End-Burning Hybrid Rocket MotorPrincipal Investigator
- Principal Investigator
  
  SOEDA KENTARO
- Project Period (FY)
  2017 – 2019
- Research Category
  
  Grant-in-Aid for Scientific Research (C)
- Research Field
  
  Aerospace engineering
- Research Institution
  The University of Tokyo

All 2022 2019 2018 2017

All Journal Article Presentation

[Journal Article] Fuel Regression Characteristics of Axial-Injection End-Burning Hybrid Rocket Using Nitrous Oxide2022
- Author(s)
  Okuda Ryota、Komizu Kodai、Tsuji Ayumu、Miwa Takumi、Fukada Mai、Yokobori Shuichi、Soeda Kentaro、Kamps Landon、Nagata Harunori
- Journal Title
  
  Journal of Propulsion and Power
  
  Volume: 38 Issue: 5 Pages: 759-770
- DOI
  10.2514/1.b38318
- Peer Reviewed
- Data Source
  KAKENHI-PROJECT-22H00240
[Journal Article] High Pressure Fuel Regression Characteristics of Axial-Injection End-Burning Hybrid Rockets2019
- Author(s)
  Saito Yuji、Kimino Masaya、Tsuji Ayumu、Okutani Yushi、Soeda Kentaro、Nagata Harunori
- Journal Title
  
  Journal of Propulsion and Power
  
  Volume: 35 Issue: 2 Pages: 328-341
- DOI
  10.2514/1.b37135
- Peer Reviewed
- Data Source
  KAKENHI-PROJECT-17K06943, KAKENHI-PROJECT-19K21064
[Journal Article] 端面燃焼式ハイブリッドロケットの推力制御時におけるヒステリシス特性に関する研究2019
- Author(s)
  君野正弥、齋藤勇士、奥谷勇士、津地歩、添田建太郎、永田晴紀
- Journal Title
  
  日本航空宇宙学会論文集
  
  Volume: 67巻、4号 Pages: 119-125
- NAID
  130007687581
- Data Source
  KAKENHI-PROJECT-17K06943
[Journal Article] Investigation of Throttling Response Characteristics of Axial-Injection End-Burning Hybrid Rockets2018
- Author(s)
  Yuji SAITO, Masaya KIMINO, Ayumu TSUJI, Kazunobu OMURA, Hiroyuki YASUKOCHI, Kentaro SOEDA, Tsuyoshi TOTANI, Masashi WAKITA, and Harunori NAGATA
- Journal Title
  
  31 ISTS Special Issue of Transaction of JSASS
  
  Volume: 16 Issue: 1 Pages: 9-18
- DOI
  10.2322/tastj.16.9
- NAID
  130006301937
- Peer Reviewed
- Data Source
  KAKENHI-PROJECT-17K06943, KAKENHI-PROJECT-17J00916
[Journal Article] Application of Axial-injection End-burning Hybrid Rockets to Small Spacecraft Propulsion2018
- Author(s)
  齋藤勇士、君野正弥、添田建太郎、戸谷剛、永田晴紀
- Journal Title
  
  Aeronautical and Space Sciences Japan
  
  Volume: 66 Issue: 10 Pages: 291-295
- DOI
  10.14822/kjsass.66.10_291
- NAID
  130007495881
- ISSN
  0021-4663, 2424-1369
- Year and Date
  2018-10-05
- Language
  Japanese
- Data Source
  KAKENHI-PROJECT-17K06943
[Journal Article] Fuel Regression Characteristics of a Novel Axial-Injection End-Burning Hybrid Rocket2017
- Author(s)
  Yuji Saito, Toshiki Yokoi, Hiroyuki Yasukochi, Kentaro Soeda, Tsuyoshi Totani, Masashi Wakita and Harunori Nagata
- Journal Title
  
  Journal of Propulsion and Power
  
  Volume: 34 Issue: 1 Pages: 247-259
- DOI
  10.2514/1.b36369
- Peer Reviewed
- Data Source
  KAKENHI-PROJECT-17K06943, KAKENHI-PROJECT-17J00916
[Journal Article] Investigation of the Throttling Characteristics of Axial-injection End-burning Hybrid Rockets2017
- Author(s)
  齋藤勇士，横井俊希，津地歩，尾村和信，安河内裕之，添田建太郎，戸谷剛，脇田督司，永田晴紀
- Journal Title
  
  JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
  
  Volume: 65 Issue: 4 Pages: 157-167
- DOI
  10.2322/jjsass.65.157
- NAID
  130005906870
- ISSN
  1344-6460, 2432-3691
- Language
  Japanese
- Peer Reviewed
- Data Source
  KAKENHI-PROJECT-17K06943, KAKENHI-PROJECT-17J00916
[Presentation] 亜酸化窒素を用いた端面燃焼式ハイブリッドロケットの推力制御特性2019
- Author(s)
  小水弘大,奥田椋太,津地歩,押見灯里, 添田建太郎,横堀秀一,永田晴紀
- Organizer
  第57回燃焼シンポジウム講演論文集
- Data Source
  KAKENHI-PROJECT-17K06943
[Presentation] 端面燃焼式ハイブリッドロケットにおける燃焼室特性長さが及ぼす c*効率への影響2019
- Author(s)
  押見灯里,津地歩,小水弘大,添田建太郎,横堀秀一, 永田晴紀
- Organizer
  第57回燃焼シンポジウム講演論文集
- Data Source
  KAKENHI-PROJECT-17K06943
[Presentation] The Accuracy of Reconstruction Techniques for Determining Hybrid Rocket Fuel Regression Rate2018
- Author(s)
  Yuji Saito, Landon Kamps, Kodai Komizu, Kentaro Soeda, Daniele Bianchi, Francesco Nasuti and Harunori Nagata
- Organizer
  54th AIAA/SAE/ASEE Joint Propulsion Conference
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-17K06943
[Presentation] Investigation of Regression Rate under High-Pressure in Axial-Injection End-Burning Hybrid Rockets2018
- Author(s)
  Yushi Okutani, Yuji Saito, Masaya Kimino, Ayumu Tsuji, Kentaro Soeda, and Harunori Nagata
- Organizer
  54th AIAA/SAE/ASEE Joint Propulsion Conference
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-17K06943
[Presentation] 端面燃焼式ハイブリッドロケットの推力制御時の時間応答性に関する研究2017
- Author(s)
  齋藤勇士，君野正弥，津地歩，尾村和信，安河内裕之，添田建太郎，戸谷剛，脇田督司，永田晴紀
- Organizer
  日本航空宇宙学会第48期年会講演会
- Data Source
  KAKENHI-PROJECT-17K06943
[Presentation] Investigation of Throttling Response Characteristics of Axial-Injection End-Burning Hybrid Rockets2017
- Author(s)
  Yuji SAITO, Masaya KIMINO, Ayumu TSUJI, Kazunobu OMURA, Hiroyuki YASUKOCHI, Kentaro SOEDA, Tsuyoshi TOTANI, Masashi WAKITA and Harunori NAGATA
- Organizer
  31st International Symposium on Space Technology and Science
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-17K06943
[Presentation] Investigation of Regression Characteristics under Relatively High-Pressure in Axial-Injection End-Burning Hybrid Rockets2017
- Author(s)
  Yuji Saito, Masaya Kimino, Ayumu Tstuji, Yushi Okutani, Hiroyuki Yashukochi, Kentaro Soeda and Harunori Nagata
- Organizer
  53rd AIAA/SAE/ASEE Joint Propulsion Conference
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-17K06943
[Presentation] 端面燃焼式ハイブリッドロケットの推力制御時におけるヒステリシス特性に関する研究2017
- Author(s)
  君野正弥，齋藤勇士，津地歩，尾村和信，安河内裕之，添田建太郎，戸谷剛，脇田督司，永田晴紀
- Organizer
  第61回宇宙科学技術連合講演会
- Data Source
  KAKENHI-PROJECT-17K06943
[Presentation] 端面燃焼式ハイブリッドロケットの宇宙機への応用2017
- Author(s)
  齋藤勇士，君野正弥，津地歩，尾村和信，安河内裕之，添田建太郎，戸谷剛，脇田督司，永田晴紀
- Organizer
  第61回宇宙科学技術連合講演会
- Data Source
  KAKENHI-PROJECT-17K06943

1. 永田晴紀 (40281787)

# of Collaborated Projects: 3 results

# of Collaborated Products: 14 results
2. Wakita Masashi (80451441)

# of Collaborated Projects: 2 results

# of Collaborated Products: 0 results
3. 田丸博晴 (30292767)

# of Collaborated Projects: 1 results

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

# of Collaborated Projects: 1 results

# of Collaborated Products: 1 results

Soeda Kentarou 添田 建太郎

SOEDA KENTARO 添田 建太郎

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

Principal Investigator

Project Period (FY)

Research Category

Review Section

Research Institution

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

Principal Investigator

Project Period (FY)

Research Category

Review Section

Research Institution

Practical use study of the Axial-Injection End-Burning Hybrid Rocket MotorPrincipal Investigator

Principal Investigator

Project Period (FY)

Research Category

Research Field

Research Institution

[Journal Article] Fuel Regression Characteristics of Axial-Injection End-Burning Hybrid Rocket Using Nitrous Oxide2022

Author(s)

Journal Title

DOI

Data Source

[Journal Article] High Pressure Fuel Regression Characteristics of Axial-Injection End-Burning Hybrid Rockets2019

Author(s)

Journal Title

DOI

Data Source

[Journal Article] 端面燃焼式ハイブリッドロケットの推力制御時におけるヒステリシス特性に関する研究2019

Author(s)

Journal Title

NAID

Data Source

[Journal Article] Investigation of Throttling Response Characteristics of Axial-Injection End-Burning Hybrid Rockets2018

Author(s)

Journal Title

DOI

NAID

Data Source

[Journal Article] Application of Axial-injection End-burning Hybrid Rockets to Small Spacecraft Propulsion2018

Author(s)

Journal Title

DOI

NAID

ISSN

Year and Date

Language

Data Source

[Journal Article] Fuel Regression Characteristics of a Novel Axial-Injection End-Burning Hybrid Rocket2017

Author(s)

Journal Title

DOI

Data Source

[Journal Article] Investigation of the Throttling Characteristics of Axial-injection End-burning Hybrid Rockets2017

Author(s)

Journal Title

DOI

NAID

ISSN

Language

Data Source

[Presentation] 亜酸化窒素を用いた端面燃焼式ハイブリッドロケットの推力制御特性2019

Author(s)

Organizer

Data Source

[Presentation] 端面燃焼式ハイブリッドロケットにおける燃焼室特性長さが及ぼす c*効率への影響2019

Author(s)

Organizer

Data Source

[Presentation] The Accuracy of Reconstruction Techniques for Determining Hybrid Rocket Fuel Regression Rate2018

Author(s)

Organizer

Data Source

[Presentation] Investigation of Regression Rate under High-Pressure in Axial-Injection End-Burning Hybrid Rockets2018

Author(s)

Soeda Kentarou 添田建太郎

SOEDA KENTARO 添田建太郎

[Presentation] 端面燃焼式ハイブリッドロケットの推力制御時の時間応答性に関する研究2017

[Presentation] 端面燃焼式ハイブリッドロケットの宇宙機への応用2017