Rchr
J-GLOBAL ID：200901019157833600   Update date: Apr. 06, 2024

HABU Hiroto

ハブ ヒロト | HABU Hiroto
Affiliation and department：
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science

About Japan Aerospace Exploration Agency Institute of Space and Astronautical Science


Job title： Professor
Other affiliations (3)：
Homepage URL  (1)： http://habu-lab.isas.jaxa.jp/
Research field  (2)： Chemical reaction and process system engineering ,  Aerospace engineering
Research keywords  (13)： SAF ,  Sounding Rocket ,  蠕動運動ミキサー ,  pyrotechnics ,  ignition ,  ionic liqid propellant ,  ionic liquid ,  固体推進薬 ,  固体ロケット推進 ,  Combustion ,  High Energy Materials ,  Solid propellants ,  Solid Propulsion
Research theme for competitive and other funds  (9)：
  • 2019 - 2024 Study on Self-compression Type Detonation Propulsion: Evolutionary Space-Flight Demonstration Study Using Sounding Rockets
  • 2015 - 2017 Technology Development of Innovative multi-function Oxygen generation from N2O
  • 2012 - 2017 Development of the fuel cell system integrated with the propulsion system for the future spacecraft
  • 2014 - 2016 The feasibility study of the advanced combined energy system using the special fuel
  • 2007 - 2010 Development of Integrated Fuel Cell Aboard Spacecraft, Operable under Ultra Low Temperature, Combined with Propulsion System
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Papers (65)：
  • Hiroki Matsunaga, Mamoru Hayata, Hiroto Habu, Masaru Noda, Atsumi Miyake. Preparation and Thermal Behavior of High Energetic Eutectic Mixture of Ammonium Dinitramide and Hydrazide Compounds. Journal of Evolving Space Activities. 2023. 1
  • Noboru Itouyama, Asato Wada, Hiroto Habu, Yoshimichi Sago. Conceptual Design of Small-Sized Thruster Using Laser Ignition of High-Energy Monopropellant. JOURNAL OF PROPULSION AND POWER. 2023. 39. 3. 416-425
  • Valentin Buyakofu, Ken Matsuoka, Koichi Matsuyama, Akira Kawasaki, Hiroaki Watanabe, Noboru Itouyama, Keisuke Goto, Kazuki Ishihara, Tomoyuki Noda, Jiro Kasahara, et al. Flight Demonstration of Pulse Detonation Engine Using Sounding Rocket S-520-31 in Space. Journal of Spacecraft and Rockets. 2023. 60. 1. 181-189
  • Keisuke Goto, Ken Matsuoka, Koichi Matsuyama, Akira Kawasaki, Hiroaki Watanabe, Noboru Itouyama, Kazuki Ishihara, Valentin Buyakofu, Tomoyuki Noda, Jiro Kasahara, et al. Space Flight Demonstration of Rotating Detonation Engine Using Sounding Rocket S-520-31. Journal of Spacecraft and Rockets. 2023. 60. 1. 273-285
  • Yuichiro Ide, Yu-ichiro Izato, Mitsuo Koshi, Atsumi Miyake, Hiroto Habu, Shinichiro Tokudome. Combustion Wave Structure of the Ammonium Dinitramide-Based Ionic Liquid Propellant. Propellants, Explosives, Pyrotechnics. 2022. 48. 2
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MISC (126)：
  • トクシュウ 「 ウツクシイホノオ 」 オ カタル. 2023. 65. 214. 220-223
  • 伊東山登, 羽生宏人, 笠原次郎. Investigation of Fundamental Operating Characteristics of Laser Radiation Heating Ignited Thrusters Using High-Energetic Ionic Liquid Propellant. 宇宙航空研究開発機構研究開発報告 JAXA-RR-(Web). 2023. 22-006
  • 矢野佑樹, 松永浩貴, 羽生宏人, 野田賢. Composition optimization of high energetic ionic liquids based on ammonium dinitramide and formohydrazide. 火薬学会春季研究発表会講演要旨集(CD-ROM). 2023. 2023
  • 松永浩貴, 伊東山登, 羽生宏人, 野田賢, 三宅淳巳. Gas generation behavior of ammonium dinitramide-based high-energy ionic liquids with catalysts. 火薬学会春季研究発表会講演要旨集(CD-ROM). 2023. 2023
  • 長町大気, 松本幸太郎, 羽生宏人. Addition of Catalysts to Solid Propellants Aiming at High Density and Low Burning Rate. 火薬学会春季研究発表会講演要旨集(CD-ROM). 2023. 2023
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Patents (22)：
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Lectures and oral presentations  (241)：
  • Development and Flight quick report of RATS (Re-entry and recovery module with deployable Aeroshell Technology for Sounding rocket experiment)
    (宇宙科学技術連合講演会講演集(CD-ROM) 2021)
  • Search of reaction condition for synthesis of ammonium dinitramide using small flow reactor
    (火薬学会春季研究発表会講演要旨集 2021)
  • Content Detection for Continuous and Efficient Production of Solid Rocket Fuel by Peristaltic Mixer
    (Proceedings of the 2020 IEEE/SICE International Symposium on System Integration, SII 2020 2020)
  • Electric ignition characteristics of an ammonium-dinitramide-based ionic liquid monopropellant with discharge plasma
    (AIAA Scitech 2020 Forum 2020)
  • Mixing and Transport Test of the Material in a Film for Continuous Solid Propellant Production using Peristaltic Mixer
    (日本機械学会ロボティクス・メカトロニクス講演会講演論文集(CD-ROM) 2020)
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Works (3)：
  • イオン液体推進薬の研究開発
    羽生 宏人 2014 - 現在
  • nanosatellite launcher SS-520-5
    Hiroto HABU 2014 - 2018
  • Lithium ejection system
    Hiroto HABU 2006 - 2011
Education (1)：
  • The University of Tokyo
Professional career (1)：
  • 博士(工学) (東京大学)
Work history (14)：
  • 2024/04 - 現在 JAXA宇宙輸送技術部門 内之浦宇宙空間観測所 所長
  • 2023/04 - 現在 Yokohama National University
  • 2023/04 - 現在 Sagami Women's University
  • 2022/12 - 現在 The University of Tokyo The Graduate School of Engineering Department of Chemical System Engineering
  • 2022/08 - 現在 Japan Aerospace Exploration Agency, Institute of Space and Astronautical Science Professor
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Awards (10)：
  • 2022/01 - JAXA宇宙科学研究所 宇宙科学研究所長賞(業績表彰・団体) 観測ロケットSS-520-3長期保管品質保証
  • 2021/06 - 一般社団法人 日本機械学会 ロボティクスメカトロニクス部門 部門優秀論文表彰 蠕動運動型混合搬送機による固体推進薬連続製造の検討
  • 2019/06 - 日本機械学会 ROBOMECH表彰(産業・実用分野) 固体推進薬の安全かつ連続的製造のための蠕動運動混合搬送装置
  • 2019/03 - 日本機械学会 宇宙工学部門一般表彰スペースフロンティア 超小型衛星打ち上げ機開発
  • 2018/04 - Guinness World Records 世界最小軌道投入ロケットSS-520-5 号機
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