Presentaion at conference, meeting, etc. - Nakata Daisuke

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  1. N2O Tank Emptying Characteristics on a Running Rocket Sled

    Kazuki Yasuda, Daisuke Nakata, Kugo Okada, Masaharu Uchiumi, Kazuyuki Higashino, Ryoji Imai，AIAA Propulsion and Energy Forum 2018，AIAA Propulsion and Energy Forum 2018 proceeding，2018.07，Cincinnati，United States

  2. ハイブリッドロケット用酸化剤タンクの自己加圧排出特性に関する研究

    安田　一貴，中田　大将，内海　政春，今井　良二，第55回伝熱シンポジウム，第55回伝熱シンポジウム予稿集，2018.05，札幌市，Japan

  3. Preliminary Experiments on Rotating Detonation Rocket Engine for Flight Demonstration Using Sounding Rocket

    Keisuke Goto, Junpei Nishimura, Junichi Higashi, Haruna Taki, Takato Ukai, Yuki Hayamizu, Hiroyuki Kikuchi, Taihei Yamada, Shun Watanabe, Koutaro Hotta, Tomoya Inakawa, Yuya Kubota, Masato Yamaguchi, Toshiki Daicho, Akira Kawasaki, Ken Matsuoka, Jiro Kasahara, Akiko Matsuo, Ikkoh Funaki, Kazuki Yasuda, Kenta Mori, Hiromitsu Yagihashi, Daisuke Nakata, Masaharu Uchiumi, Kazuyuki Higashino，AIAA Scitech 2018，AIAA Scitech 2018 proceeding，2018.01，Kissimmee，United States

  4. Analytical and Experimental Study of Compressor Performance for Gas Generator Cycle Air Turbo Ramjet Engine

    Ryojiro Minato, Ryoji Imai, Kazuyuki Higashino, Daisuke Nakata, and Mayu Ishihara ，ISABE2017 Conference，ISABE2017 Conference proceeding，2017.09，United Kingdom

  5. Sea Level Static Tests of Gas Generator Cycle Air Turbo Ramjet Engine for Supersonic UAV

    Kazuyuki Higashino, Daisuke Nakata, Ryojiro Minato, Ryoji Imai, Nobuhiro Tanatsugu, Yuta Yashima, and Hiroto Mukae，ISABE2017 Conference，ISABE2017 Conference proceeding，2017.09，United Kingdom

  6. N2O Flow History Prediction in an Oxidizer Feed Line of Hybrid Rockets

    Daisuke Nakata, Kazuki, Yasuda, Kugo Okada, Kazuyuki Higashino and Rikio Watanabe，31st International Symposium on Space Science and Technology，31st International Symposium on Space Science and Technology proceeding，2017.06，Japan

  7. ハイブリッドロケットのクラスタリングに関する基礎研究

    安田 一貴, 中田 大将, 岡田 空悟, 東野 和幸, 廣田 光智, 渡邉 力夫，第60回宇宙科学技術連合講演会，第60回宇宙科学技術連合講演会講演集，2016.09，函館市，Japan

  8. A Fundamental Study on the Hybrid Clustering for the Rocket Sled Propulsion System

    Daisuke Nakata, Kazuki Yasuda, Shuhei Horio, Kazuyuki Higashino，Propulsion and Energy Forum and Exposition，AIAA Paper，2016.07，Salt Lake City，United States

  9. Study on the Thermal Deomposition of Bioetanol as a High-Pressure Rocket Propellant

    Asuka Iijima, Daisuke Nakata,Kazuyuki Higashino，Propulsion and Energy Forum and Exposition，AIAA Paper，2016.07，Salt Lake City，United States

  10. ロケットのクラスタリングに関する一考察

    中田大将，宇宙輸送シンポジウム，宇宙輸送シンポジウム講演集，2016.01

  11. 高速走行軌道実験設備

    中田大将、棚次亘弘、東野和幸，第52回飛行機シンポジウム，2014.10

  12. Development of Long-life Lightweight Arcjets

    Daisuke Nakata, Kiyoshi Kinefuchi, Satoshi Hosoda, Masahiro Kinoshita, Hirokazu Tahara, Hitoshi Kuninaka，The 33rd International Electric Propulsion Conference，2013.10，Washington D.C.，United States

  13. Experimental Study of Hollow CathodesApplication to DC Arcjet

    Masahiro Kinoshita, Daisuke Nakata, Kiyoshi Kinefuchi, Hitoshi Kuninaka，The 33rd International Electric Propulsion Conference，2013.10，Washington D.C.，United States

  14. Rocket Sled Track Facility as a Test Platform and Launch Assist of Space Planes

    Daisuke Nakata, Nobuhiro Tanatsugu, Kazuyuki Higashino, Ken Higuchi, Takeshi Tsuchiya and Takehiro Himeno，Ground Based Space Facility conference，2013.06，Paris，France

  15. Aerodynamic Measurement on the High Speed Test Track

    Daisuke Nakata, Kenji Nishine, Kaoru Tateoke, Kazuyuki Higashino, Nobuhiro Tanatsugu，The 29th International Symposium on Space Technology and Science，2013.06，Nagoya，Japan

  16. Research and Development of High Speed Test Track Facility in Japan

    Daisuke Nakata, Jun Yajima, Kenji Nishine, Kazuyuki Higashino and Nobuhiro Tanatsugu，AIAA Science Meeting 2012，2012.01，Nashbille，United States

  17. Thermal Stress Analysis of Several Hundred kW Radiation Cooled Arcjet

    Daisuke Nakata, Kiyoshi Kinefuchi, Hitoshi Kuninaka, “Thermal Stress Analysis of Several Hundred kW Radiation Cooled Arcjet，32nd International Electric Propulsion Conference，2011.09，Wiesbaden，Germany

  18. Predicted and Experimented Acceleration Profile of the Rocket Sled

    Daisuke Nakata, Ami Kozu, Jun Yajima, Kenji Nishine, Kazuyuki Higashino and Nobuhiro Tanatsugu，The 28th International Symposium on Space Technology and Science，2011.06，Okinawa，Japan

  19. Voltage Hash of Various Propellants in Self-Field Magnetoplasmadynamic Thrusters

    Daisuke Nakata, Kyoichiro Toki, Yukio Shimizu, Hitoshi Kuninaka，31st International Electric Propulsion Conference，31st International Electric Propulsion Conference，2009.09，Ann Arbor，United States

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