Curriculum Vitaes
  1. Researcher Search Results
  2. Hiroaki Kobayashi

Hiroaki Kobayashi

  (小林 弘明)

Profile Information

Affiliation
Professor, Institute of Space and Astronautical Science, JAXA
Degree
工学博士(東京大学)
J-GLOBAL ID
200901061542880861
researchmap Member ID
5000019456

Research Areas

 1

Research History

 8
More

Education

 1

Committee Memberships

 2

Papers

 180
More

Misc.

 10
  • 井田基紀, 坂本勇樹, 伊藤千珠, 中山才誠, 真子弘泰, 八木邑麿, 山田和彦, 丸祐介, 小林弘明, 徳留真一郎, 徳留真一郎
    日本伝熱シンポジウム講演論文集(Web), 62nd, 2025  
  • 丸祐介, 坂本勇樹, 小林弘明, 徳留真一郎, 三浦政司, 大山聖, 野中聡, 澤井秀次郎, 佐藤哲也
    日本機械学会年次大会講演論文集(CD-ROM), 2025, 2025  
  • TOKUDOME, Shinichiro, NONAKA, Satoshi, KOBAYASHI, Hiroaki, MARU, Yusuke, MIURA, Masashi, SAKAMOTO, Yuki, YAMADA, Tetsuya, USUKI, Tomoaki
    Proceedings of Sounding Rocket Symposium 2023, Feb, 2024  
  • 野中, 聡, 小林, 弘明, NONAKA, Satoshi, KOBAYASHI, Hiroaki
    観測ロケットシンポジウム2022 講演集 = Proceedings of Sounding Rocket Symposium 2022, Mar, 2023  
    第5回観測ロケットシンポジウム(2023年2月28日-3月1日. オンライン開催) 5th Sounding Rocket Symposium(February 28-March 1, 2023. Online Meeting) 資料番号: SA6000185034 レポート番号: Ⅵ-6 【招待講演】
  • 小林, 弘明, 坂本, 勇樹, 丸, 祐介, 徳留, 真一郎, 野中, 聡, 澤井, 秀次郎, 佐藤, 哲也, KOBAYASHI, Hiroaki, SAKAMOTO, Yuki, MARU, Yusuke, TOKUDOME, Shinichiro, NONAKA, Satoshi, SAWAI, Shujiro, SATO, Tetsuya
    観測ロケットシンポジウム2020 講演集 = Proceedings of Sounding Rocket Symposium 2020, Mar, 2021  
    第3回観測ロケットシンポジウム（2021年3月24-25日. オンライン開催) 3rd Sounding Rocket Symposium (March 24-25, 2021. Online Meeting) PDF再処理の為、2023年3月17日に差替 資料番号: SA6000162015 レポート番号: Ⅴ-1
  • 丸, 祐介, 佐藤, 哲也, 小林, 弘明, 徳留, 真一郎, 野中, 聡, 澤井, 秀次郎, Maru, Yusuke, Sato, Tetsuya, Kobayashi, Hiroaki, Tokudome, Shinichiro, Nonaka, Satoshi, Sawai, Shujiro
    観測ロケットシンポジウム2019 講演集 = Proceedings of Sounding Rocket Symposium 2019, Aug, 2019  
    第2回観測ロケットシンポジウム（2019年8月5日-6日. 宇宙航空研究開発機構宇宙科学研究所（JAXA)(ISAS)）, 相模原市, 神奈川県 2nd Sounding Rocket Symposium (August 5-6, 2019. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan 資料番号: SA6000142004 レポート番号: Ⅰ-4
  • 小林, 弘明, 成尾, 芳博, 丸, 祐介, 竹崎, 悠一郎, 杉野, 伸也, 野中, 聡, 八木下, 剛, 大門, 優, 谷, 洋海, 梅村, 悠, 武藤, 大貴, 松本, 万有, 辻上, 博司, 宮鍋, 昂大, 吉野, 裕, 河村, 哲, Kobayashi, Hiroaki, Naruo, Yoshihiro, Maru, Yusuke, Takesaki, Yuichiro, Sugino, Shinya, Sato, Mamoru, Yagishita, Tsuyoshi, Daimon, Yu, Tani, Hiroumi, Umemura, Yutaka, Muto, Daiki, Matsumoto, Mayu, Tsujigami, Hiroshi, Miyanabe, Kota, Yoshino, Yuu, Kawamura, Satoru
    平成29年度宇宙輸送シンポジウム: 講演集録 = Proceedings of Space Transportation Symposium FY2017, Jan, 2018  
    平成29年度宇宙輸送シンポジウム（2018年1月18日-19日. 宇宙航空研究開発機構宇宙科学研究所（JAXA)(ISAS)）, 相模原市, 神奈川県 Space Transportation Symposium FY2017 (January 18-19, 2018. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan 資料番号: SA6000210024 レポート番号: STCP-2017-024
  • SAWAI Shujiro, FUJITA Kazuhisa, KOBAYASHI Hiroaki, SAKAI Shin’ichiro, BANDO Nobutaka, KADOOKA Shouhei, TSUBOI Nobuyuki, MIYAJI Koji, UCHIYAMA Taku, HASHIMOTO Tatsuaki
    Transactions of the Japan Society for Aeronautical and Space Sciences, Space Technology Japan (Web), 7(ists26) Tg_27-Tg_34, 2009  
    JAXA is developing Mach 5 hypersonic turbojet engine technology that can be applied in a future hypersonic transport. Now, Jet Engine Technology Research Center of JAXA conducts the experimental study using a 1 / 10 scale-model engine. In parallel to engine development activities, a new supersonic flight-testing vehicle for the hypersonic turbojet engine is under development since 2004. In this paper, the system configuration of the flight-testing vehicle is outlined and development status is reported.
  • ISHIKAWA Takehiko, HASHIMOTO Tatsuaki, SAWAI Shujiro, SAITO Yoshitaka, INATOMI Yuko, YOSHIMITSU Tetsuo, SAKAI Shin’ichiro, KOBAYASHI Hiroaki, FUJITA Kazuhisa, BANDO Nobutaka
    Transactions of the Japan Society for Aeronautical and Space Sciences, Space Technology Japan (Web), 7(ists26) Ph_29-Ph_33, 2009  
    The second flight of microgravity experiment system using a free fall capsule from a high altitude balloon was conducted in May 2007. Using a drag free control, around 10-4G gravity conditions were obtained for 30 seconds. Results of a combustion experiment with Japanese sparker conducted inside the microgravity experimental unit were also reported.
  • Kobayashi, Hiroaki, Sawai, Shujiro, Sawai, Shujiro, Taguchi, Hideyuki, Kojima, Takayuki, Fukiba, Katsuyoshi, Fujita, Kazuhisa, Fujita, Kazuhisa, Sato, Tetsuya, Sato, Tetsuya
    15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2008  
    JAXA is developing Mach 5 hypersonic turbojet engine technology that can be applied in a future hypersonic transport. Now, in Jet Engine Technology Research Center of JAXA, the experimental study, which uses a 1 / 10 scale-model engine, is conducted. In parallel to engine development activities, a new supersonic flight-testing vehicle for the hypersonic turbojet engine is under development since 2004. In this paper, the system configuration of the flight-testing vehicle is outlined and development status is reported.

Presentations

 198
More

Professional Memberships

 3

Research Projects

 10
More

Industrial Property Rights

 9
More
To the list screen