International conference proceedings - Nakata Daisuke

21. In-Space Flight Demonstration Results of a Detonation Engine System on Sounding Rocket S-520-31: Pulse Detonation Engine

    V. Buyakofu, K. Matsuoka, K. Matsuyama, K. Goto, A. Kawasaki, H. Watanabe, N. Itouyama, K. Ishihara, T. Noda, J. Kasahara, A Matsuo, I. Funaki, D. Nakata, M. Uchiumi, H. Habu, S. Takeuchi, S. Arakawa, J. Masuda, K. Maehara, Y. Kazuhiko, T. Nakao，33rd International Symposium on Space Technology and Science Proceedings，2022.02

    

22. Experimental Study on Filling and Discharging Characteristics of Nitrous Oxide to Spacecraft Tanks

    Kazuki Yasuda, Tatsuhiko Shiina, Daisuke Nakata, Masaharu Uchiumi，33rd International Symposium on Space Technology and Science，2022.02

    

23. Experimental Investigation of Hybrid Rocket Acoustics

    Shintaro Nakamura, Mikiya Araki, Juan C. González Palencia, Koki Yamagishi, Kazuki Yasuda, Daisuke Nakata, Masaharu Uchiumi，33rd International Symposium on Space Technology and Science Proceedings，2022.02

    

24. Performance Characteristics of High-Thrust High-specific-Impulse Steady-State Magneto-Plasma-Dynamic Thrusters for Transportation in the Solar System -Use of Carbon Dioxide, Methane, Ammonia, Hydrogen, Helium, Air and Water/Ice etc. in the Planets and Satellites to Propellants

    Ayano Yoshida, Ryo Ikemoto, Kazuki Shibutani, Kentaro Kaji, Hirokazu Tahara, Ai Momozawa, Daisuke Nakata, Tomoyuki Ikeda, Yoshiyuki Takao, Takashi Wakizono, Masaya Toyama，33rd International Symposium on Space Technology and Science Proceedings，2022.02

    

25. Performance Characteristics of DC Arcjet Thrusters -Use of Carbon Dioxide, Methane, Ammonia, Hydrogen, Helium, Air and Water/Ice etc. in Planets and Satellites in the Solar System to Propellants

    Kentaro Kaji, Kazuki Shibutani, Ryo Ikemoto, Ayano Yoshida, Hirokazu Tahara, Ai Momozawa, Daisuke Nakata, Tomoyuki Ikeda, Yoshiyuki Takao, Yuichiro Nogawa, Takashi Wakizono, Masaya Toyama，33rd International Symposium on Space Technology and Science Proceedings，2022.02

    

26. Rocket Sled System Design for Various Missions

    Daisuke Nakata, Kazuki Yasuda, Akihiro Watanabe, Ang YiYong, Koki Yamagishi, Tatsuhiko Shiina, Takuya Tada, Iori Obara, Yuma Hashimoto, Hikaru Eguchi, Masaharu Uchiumi，33rd International Symposium on Space Technology and Science Proceedings，2022.02

    

27. Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Pulse Detonation Engine

    V. Buyakofu, K. Matsuoka, K. Matsuyama, K. Goto, A. Kawasaki, H. Watanabe, N. Itouyama, K. Ishihara, T. Noda, J. Kasahara, A. Matsuo, I. Funaki, D. Nakata, M. Uchiumi, H. Habu, S. Takeuchi, S. Arakawa, J. Masuda, K. Maehara, T. Nakao, K. Yamada，AIAA Scitech2022，Article Number:AIAA 2022-0233，2022.01

    

28. Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: System Design

    A. Kawasaki, K. Matsuyama, K. Matsuoka, H. Watanabe, N. Itouyama, K. Goto, K. Ishihara, V. Buyakofu., T. Noda, J. Kasahara, A. Matsuo, F. Funaki, D. Nakata, M. Uchiumi, H. Habu, S. Takeuchi, S. Arakawa, J. Masuda, K. Maehara, T. Nakao, K. Yamada，AIAA SciTech 2022 Proceedings，Article Number:AIAA-2022-0229，2022.01

    

29. Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: History from Development to Flight

    N. Itouyama, K. Matsuyama, K. Matsuoka, A. Kawasaki, H. Watanabe, K. Goto, K. Ishihara, V. Buyakofu, T. Noda, J. Kasahara, A. Matsuo, I. Funaki, D. Nakata, M. Uchiumi, H. Habu, S. Takeuchi, S. Arakawa, J. Masuda, K. Maehara, T. Nakao, K. Yamada，AIAA SciTech 2022 Proceedings，Article Number:AIAA 2022-0230，2022.01

    

30. Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Flight Path and Attitude

    H. Watanabe, K. Matsuyama, K. Matsuoka, A. Kawasaki, N. Itouyama, K. Goto, K. Ishihara, V. Buyakofu, T. Noda, S. Ito, J. Kasahara, A. Matsuo, I. Funaki, D. Nakata, M. Uchiumi, H. Habu, S. Takeuchi, S. Arakawa, J. Masuda, K. Maehara, T. Nakao, K. Yamada，AIAA SciTech 2022，Article Number:AIAA 2022-0231，2022.01

    

31. Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-31: Performance of Rotating Detonation Engine

    K. Goto, K. Matsuoka, K. Matsuyama, A. Kawasaki, H. Watanabe, N. Itouyama, K. Ishihara, V. Buyakofu, T. Noda, J. Kasahara, A. Matsuo, I. Funaki, D. Nakata, M. Uchiumi, H. Habu, S. Takeuchi, S. Arakawa, J. Masuda, K. Maehara, T. Nakao, K. Yamada，AIAA SciTech 2022 Proceedings，Article Number:AIAA 2022-0232，2022.01

    

32. Experimental Study on Visualization of Gas-liquid Two-phaes Flow with Self-pressurization of Nitrous Oxide for Rocket Propellants

    Kazuki YASUDA, Daisuke NAKATA, Ryoji IMAI, Masaharu UCHIUMI，7th Edition of the Space Propulsion Conference，2021.03

    

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

    Kazuki YASUDA, Daisuke NAKATA, Masaharu UCHIUMI，18th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery，2020.11

    

34. Hot Gas Temperature Distribution in a Gas-Generator for Air Turbo Ramjet Engine

    Daisuke Nakata, Ryojiro Minato, Hiromitsu Yagihashi, Koki Arimatsu, Inaho Yoshikawa, Satoshi Inazumi, Masaya Sumiyoshi, Masaharu Uchiumi，24th ISABE conference，2019.09

    

35. Dual Manifold Flow Control System for Gas-Generator Cycle Air Ramjet Engine

    Ryojiro Minato, Daisuke Nakata, Masaharu Uchiumi, Inaho, Yoshikawa, Hiromitsu, Yagihashi and Kouki Arimatsu，24th ISABE conference，2019.09

    

36. Propulsive Performance of Rotating Detonation Engines in CH4/O2 and C2H4/O2 for Flight Experiment

    Keisuke Goto, Akira Kawasaki, Ken Matsuoka, Jiro Kasahara, Akiko Matsuo, Daisuke Nakata, Ryuya Yokoo, Juhoe Kim, Ikkoh Funaki, Masaharu Uchiumi, Hideto Kawashima，The 27th ICDERS，2019.08

    

37. THE MINIMUM FLOW RATE OF LIQUID-OXYGEN WHEN CONSIDERING A THROTTLING OF A GAS GENERATOR CYCLE ENGINE

    Daisuke Nakata, Ryojiro Minato, Inaho Yoshikawa, Hiromitsu Yagihashi, Koki Arimatsu and Masaharu Uchiumi，ASME-JSME-KSME 2019 Joint Fluids Engineering Conference AJKFLUIDS2019，2019.07

    

38. FUNDAMENTAL STUDY ON INJECTOR FLOW HARACTERISTICS OF SELF-PRESSURIZING FLUID FOR SMALL ROCKET ENGINES

    Kazuki YASUDA, Daisuke NAKATA, Masaharu UCHIUMI, Kugo OKADA, Ryoji IMAI，ASME-JSME-KSME 2019 Joint Fluids Engineering Conference AJKFLUIDS2019，2019.07

    

39. EXPERIMENTAL STUDY OF TEMPERATURE AND PHASE TRANSITION OF LIQUID OXYGEN AT IGNITION IN IMPINGING INJECTOR OF GAS GENERATOR

    Hiromitsu Yagihashi, Daisuke Nakata, Ryojiro Minato, Inaho Yoshikawa, Koki Arimatsu, Masaharu Uchiumi，ASME-JSME-KSME 2019 Joint Fluids Engineering Conference AJKFLUIDS2019，2019.07

    

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

    Koki Arimatsu, Daisuke Nakata, Ryojiro Minato, Inaho Yoshikawa, Hiromitsu Yagihashi, Masaharu Uchiumi，32nd International Symposium on Space Technology and Science，2019.06