Papers - Nakata Daisuke

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  1. Nitrous Oxide/Ethanol Cylindrical Rotating Detonation Engine for Sounding Rocket Space Flight

    Kazuki Ishihara, Tomoki Sato, Tomoaki Kimura, Kosuke Nakajima, Kotaro Nakata, Noboru Itouyama, Akira Kawasaki, Ken Matsuoka, Koichi Matsuyama, Jiro Kasahara, Hikaru Eguchi, Daisuke Nakata, Masaharu Uchiumi, Akiko Matsuo, Ikkoh Funaki，JOURNAL OF SPACECRAFT AND ROCKETS，vol.Vol. 62，(No. 1)，(p.44 ～ 54)，2025.01

  2. Flow-Pattern Identification and Pressure-Drop Measurement in a Self-pressurized Flow of Nitrous Oxide

    Takuya TADA, Kazuki YASUDA, Hiro OKANO, Hikaru EGUCHI, Masaharu UCHIUMI, Daisuke NAKATA,，Trans. Japan Soc. Aero. Space Sci.，vol.Vol. 67，(No. 6)，(p.318 ～ 326)，2024.11

  3. Experimental Parameter Identification and an Evaluation of the Impact of Tire Models on the Dynamics of Fixed-Wing Unmanned Aerial Vehicles

    Hikaru Eguchi, Daisuke Nakata，Aerospace，vol.11，(8)，2024.07

  4. Combustion Structure of a Cylindrical Rotating Detonation Engine with Liquid Ethanol and Nitrous Oxide

    Tomoki Sato, Kotaro Nakata, Kazuki Ishihara, Noboru Itouyama, Ken Matsuoka, Jiro Kasahara, Akira Kawasaki, Daisuke Nakata, Hikaru Eguchi, Masaharu Uchiumi, Akiko Matsuo, Ikkoh Funaki，Combustion and Flame，2024.06

  5. Estimation of the Heat Generation of the Metal Composite Powder Absorbing the Pulsed Flow of Hydrogen Gas

    Tomotaka Kobayashi, Ken Naitoh, Daiki Okada, Ryuki Nakagawa, Yuta Toba, Masaharu Uchiumi, Daisuke Nakata，J. Condensed Matter Nucl. Sci，vol.38，(p.96 ～ 107)，2024.05

  6. Flight Demonstration of Pulse Detonation Engine Using Sounding Rocket S-520-31 in Space

    Valentin Buyakofu, Ken Matsuoka, Koichi Matsuyama, Akira Kawasaki, Hiroaki Watanabe, Noboru Itouyama, Keisuke Goto, Kazuki Ishihara, Tomoyuki Noda, Jiro Kasahara , Akiko Matsuo, Ikkoh Funaki, Daisuke Nakata, Masaharu Uchiumi, Hiroto Habu, Shinsuke Takeuchi, Satoshi Arakawa, Junichi Masuda, Kenji Maehara, Tatsuro Nakao and Kazuhiko Yamada，Journal of Spacecraft and Rockets，vol.60，(1)，2023.01

  7. Space flight demonstration of rotating detonation engine using sounding rocket S-520-31

    Keisuke Goto, Ken Matsuoka, Koichi Matsuyama, Akira Kawasaki, Hiroaki Watanabe, Noboru Itouyama, Kazuki Ishihara, Valentin Buyakofu, Tomoyuki Noda, Jiro Kasahara , Akiko Matsuo, Ikkoh Funaki, Daisuke Nakata, Masaharu Uchiumi, Hiroto Habu, Shinsuke Takeuchi, Satoshi Arakawa, Junichi Masuda, Kenji Maehara, Tatsuro Nakao and Kazuhiko Yamada，Journal of Spacecraft and Rockets，vol.60，(1)，(p.273 ～ 285)，2023.01

  8. Space flight demonstration of rotating detonation engine using sounding rocket S-520-31

    Goto, Keisuke; Matsuoka, Ken; Matsuyama, Koichi; Kawasaki, Akira; Watanabe, Hiroaki; Itouyama, Noboru; Ishihara, Kazuki; Buyakofu, Valentin; Noda, Tomoyuki; Kasahara, Jiro，Journal of Spacecraft and Rockets，vol.60，(1)，(p.273 ～ 285)，2023.01

  9. Overspeeding Characteristics of Turbomachinery for Gas Generator Cycle Air Turbo Ramjet Engine

    Ryojiro Minato, Daisuke Nakata, Masaharu Uchiumi, Ryoji Imai, Kazuyuki Higashino，Propulsion and Power Research，vol.11，(4)，(p.444 ～ 456)，2022.12

  10. Effect of the fabrication process on the microstructural evolution of carbon fibers and flexural property on C/SiC composites by the NITE method

    Sang-Hyun Jung, Hirotatsu Kishimoto, Naofumi Nakazato, Daisuke Nakata, Joon-Soo Park, Akira Kohyama，Ceramics International，vol.48，(p.f ～ 32722)，2022.11

  11. Effect of the fabrication process on the microstructural evolution of carbon fibers and flexural property on C/SiC composites by the NITE method

    Sang-Hyun Jung, Hirotatsu Kishimoto, Naofumi Nakazato, Daisuke Nakata, Joon-Soo Park, Akira Kohyama，Ceramics International，vol.48，(p.32712 ～ 32722)，2022.11

  12. Thermal Design and Experimental Verification of a 3D-Printed Resistojet

    Daisuke Nakata, Kiyoshi Kinefuchi, Hitoshi Sakai and Suyalatu，Journal of Propulsion and Power，vol.38，(1)，(p.148 ～ 156)，2022.01

  13. Development of an S-Shaped Pulse Detonation Engine for a Sounding Rocket

    Valentin Buyakofu, Ken Matsuoka, Koichi Matsuyama, Akira Kawasaki, Hiroaki Watanabe, Noboru Itouyama, Keisuke Goto, Kazuki Ishihara, Tomoyuki Noda, and Jiro Kasahara, Akiko Matsuo, Ikkoh Funaki, Daisuke Nakata, Masaharu Uchiumi, Hiroto Habu, Shinsuke Takeuchi, Satoshi Arakawa, Junichi Masuda and Kenji Maehara，Journal of Spacecraft and Rockets，2022.01

  14. Study on Propellant Supply System for a Small-scale Supersonic Flight Experiment Vehicle (Study on a Propellant Management Device)

    Naoki SOTA, Ryoji IMAI, Aoki ANADA, Taisei YAMAZAKI, Masaharu UCHIUMI,Daisuke NAKATA, and Ryojiro MINATO，International Journal of Microgravity Science and Application，vol.39，(1)，2022.01

  15. Additive-manufactured single-piece thin multi-layer tungsten heater for an electrothermal thruster

    Kiyoshi Kinefuchi, Daisuke Nakata, Giulio Coral, Suyalatu, Hitoshi Sakai, Tsukizaki Ryudo and Kazutaka Nishiyama，Review of Scientific Instruments，vol.92，(11)，2021.11

  16. Experimental Study on Temperature Change by Cavitation accompanying Self-pressurization of Propellant for Small Rocket Engines

    Yasuda K, Nakata D. and Uchiumi M.，JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME，vol.143，(12)，2021.07

  17. Design and testing of additively manufactured high-efficiency resistojet on hydrogen propellant

    G. Coral, K. Kinefuchi, D. Nakata, R. Tsukizaki, K. Nishiyama, H. Kuninaka，Acta Astronautica，2021.04

  18. On the Pressure Loss Characteristics of Liquid Oxygen Considering a Heat Input

    Koki Arimatsu, Daisuke Nakata, Ryojiro Minato, Inaho Yoshikawa, Hiromitsu Yagihashi and Masaharu Uchiumi，Transactions of the Japan Society for Aeronautical and Space Sciences，vol.19，(2)，(p.217 ～ 223)，2021.03

  19. Fundamental Study on Injector Flow Characteristics of Self-Pressurizing Fluid for Small Rocket Engines

    Kazuki Yasuda, Daisuke Nakata, Masaharu Uchiumi, Kugo Okada and Ryoji Imai，JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME，vol.143，(2)，2021.02

  20. Thrust Validation of Rotating Detonation Engine System by Moving Rocket Sled Test

    Keisuke Goto, Yuichi Kato, Kazuki Ishihara, Ken Matsuoka, Jiro Kasahara, Akiko Matsuo, Ikkoh Funaki, Daisuke Nakata, Kazuyuki Higashino and Nobuhiro Tanatsugu，Journal of Propulsion and Power，2020.12

  21. 小型超音速機用エンジンの定常軸振動解析による危険速度通過時の軸振動評価

    橋本啓吾，向江洋人，湊亮二郎，中田大将，内海政春，ターボ機械，vol.48，(4)，(p.208 ～ 215)，2020.04

  22. Study on Propellant Supply System for Small-scale Supersonic Flight Experiment Vehicle (Development of LOX Supply System design technology)

    Yukiya SATO, Ryoji IMAI, Daisuke NAKATA, Ryojiro MINATO, Masaharu UCHIUMI，International Journal of Microgravity Science and Application，vol.37，(1)，(p.370104-1 ～ 370104-7)，2020.01

  23. Experimental Propulsive Performance and Heating Environment of Rotating Detonation Engine with Various Throat Geometries

    Goto Keisuke, Nishimura Junpei, Kawasaki Akira, Matsuoka Ken, Kasahara Jiro, Matsuo Akiko, Funaki Ikkoh, Nakata Daisuke, Uchiumi Masaharu, Higashino Kazuyuki，Journal of Propulsion and Power，vol.35，(1)，(p.213 ～ 223)，2019.01

  24. 小型超音速機エンジン用玉軸受の発熱／冷却特性評価

    向江 洋人，石原 眞優，湊 亮二郎，中田 大将，東野 和幸, 内海 政春，ターボ機械，vol.46，(6)，(p.331 ～ 337)，2018.06

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

    Daisuke Nakata, Kazuki, Yasuda, Kugo Okada, Kazuyuki Higashino and Rikio Watanabe，Transaction of JSASS, Aerospace Technology Japan，vol.16，(1)，(p.81 ～ 87)，2018.01

  26. 再生冷却システムに用いる熱分解吸熱性燃料に対するニッケルおよびプラチナ触媒の効果

    塚野 徹，前田大輔，笹山容資，中田大将，杉岡正敏，棚次亘弘，東野和幸，日本航空宇宙学会論文集，vol.65，(2)，2017.04

  27. Rocket Engine Feasibility Study for the JAXA Future Transportation Reference System

    Asuka Iijima, Daisuke Nakata, Masatoshi Sugioka, Nobuhiro Tanatsugu, Kazuyuki Higashino, Shinji Ishimoto, Nobuyuki Azuma，Aerospace Technology Japan，vol.14，(ists30)，(p.Po_1_17 ～ Po_1_23)，2017.02

  28. Technical Challengers for Advanced Arcjets

    Daisuke Nakata, Kiyoshi Kinefuchi，Satoshi Hosoda, Masahiro Kinoshita and Hitoshi Kuninaka，Aerospace Technology Japan，vol.12，(ists29)，(p.To_1_1-To_1_5 ～ )，2014.11

  29. Aerodynamic Measurement on the High Speed Test Track

    Daisuke Nakata, Kenji Nishine, Kaoru Tateoke, Nobuhiro Tanatsugu　and Kazuyuki Higashino，Aerospace Technology Japan，vol.12，(ists29)，(p.Tg_5-Tg_10 ～ )，2014.07

  30. Development of a Small-scale Supersonic Flight Experiment Vehicle as a Flying Test Bed for Future Space Transportation Research

    Kazuhide Mizobata, Ryojiro Minato, Ken Higuchi, Masazumi Ueba, Syohei Takagi, Daisuke Nakata, Kazuyuki Higashino and Nobuhiro Tanatsugu，Aerospace Technology Japan，vol.12，(ists29)，(p.Po_3_1-Po_3_10 ～ )，2014.07

  31. Predicted and Experimented Acceleration Profile of the Rocket Sled

    Daisuke Nakata, Ami Kozu, Jun Yajima, Kenji Nishine, Kazuyuki Higashino and Nobuhiro Tanatsugu，Aerospace Technology Japan，vol.10，(ists28)，(p.Ta_1-Ta_5 ～ )，2012.03

  32. Performance of ThO2-W, Y2O3-W and La2O3-W cathodes in Quasi-Steady Magnetoplasmadynamic Thrusters

    Daisuke Nakata, Kyoichiro Toki, Ikkoh Funaki, Hitoshi Kuninaka，Journal of Propulsion and Power，vol.27，(4)，(p.912 ～ 915)，2011.08

  33. Experimental Study of a Two-Dimensional Applied Field Magnetoplasmadynamic Thruster

    Akira Iwakawa, Daisuke Nakata and Hitoshi Kuninaka，Aerospace Technology Japan，vol.8，(ists27)，(p.Pb13-Pb17 ～ )，2010.12

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