International conference proceedings - Nakata Daisuke

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  1. Turbine Supply Gas Temperature Equalization in a Gas Generator Cycle Air Turbo Ramjet Engine

    Daisuke Nakata, Akitomo Fujiura, Mio Namera, Naoki Hanawa, Ryojiro Minato, Hikaru Eguchi, Masaharu Uchiumi，ISABE Conferencee 2024，2024.09

  2. Flight Demonstration of Detonation Engine System Using Sounding Rocket S-520-34:Performance of Rotating Detonation Engine Using Liquid Propellants

    Tomoki Sato, Ken Matsuoka, Noboru Itouyama, Masaaki Yasui, Koichi Matsuyama, Yuichiro Ide, Kotaro Nakata, Yamato Suzuki, Ryoto Ishibashi, Sota Suzuki, Jiro Kasahara, Akira Kawasaki, Hidetoshi Hirashima, Daisuke Nakata, Hikaru Eguchi, Tomoyuki Takano, Masaharu Uchiumi, Akiko Matsuo, Ikkoh Funaki, Hiroto Habu, Satoshi Arakawa, Junichi Masuda, Kosuke Kawahara, Tomoaki Usuki, Kenji Maehara, Maki Shida, Tatsuro Nakao, Kazuhiko Yamada, Takehiro Himeno, Yusei Yahata，AIAA SciTech Forum，2025.01

  3. Application and Testing of Nitromethane Monopropellant - From Rocket to Air-Breathing Engine

    Ryojiro Minato, Daisuke Nakata, Shuichi Nakamura, Kazuyuki Higashino，ISABE Conferencee 2024，2024.09

  4. Study of Low-Speed Aerodynamic Performance of a Supersonic Intake

    Ryo Kambara, Ryojiro Minato, Daisuke Nakata，ISABE Conferencee 2024，2024.09

  5. PROGRESS OF SUB-SCALE FLIGHT TESTS PLAN WITH ATRIUM ENGINE

    Yuki Sakamoto, Hiroaki Kobayashi, Yusuke Maru, Shinichiro Tokudome, Akira Oyama, Shinsuke Takeuchi, Masashi Miura, Daisaku Masaki, Satoshi Takada, Hiromitsu Kakudo, Toru Kaga, Ryoma Yamashiro, Kiyoshi Kinufuchi, Hiroyasu Manako, Masaharu Uchiumi, Dasuke Nakata, Hikaru Eguchi, Ryojiro Minato, Katsuyoshi Fukiba, Akira Kawasaki, Shinichi Maeda, Yoichi Takeda, Tetsuya Sato，SPACE PROPULSION，2024.05

  6. Operation Characteristics of Cylindrical Rotating Detonation Engine Using Liquid Ethanol and Liquid Nitrous Oxide

    Tomoki Sato, Kotaro Nakata, Satoru Sawada, Yamato Suzuki, Yusuke Kudo, Kosuke Nakajima, Noboru Itouyama, Ken Matsuoka, Jiro Kasahara, Akira Kawasaki, Mio Namera, Hikaru Eguchi, Daisuke Nakata, Masaharu Uchiumi, Akiko Matsuo, Ikkoh Funaki，2024 AIAA SciTech，2024.01

  7. Overview for the research and development of Rotating Detonation Engine Systems using a liquid-liquid propellant combination

    Noboru Itouyama, Koichi Matsuyama, Ken Matsuoka, Tomoki Sato, Kotaro Nakata, Satoru Sawada, Yusuke Kudo, Kosuke Nakajima, Yamato Suzuki, Jiro Kasahara, Akira Kawasaki, Mio Namera, Daisuke Nakata, Hikaru Eguchi, Masaharu Uchiumi, Akiko Matsuo, Ikkoh Funaki，2024 AIAA SciTech，2024.01

  8. A Bread Board Model Testing for In-Space Flight Demonstration of a Liquid-Propellant Detonation Engine System

    Akira Kawasaki, Kotaro Nakata,Tomoki Sato, Satoru Sawada, Yusuke Kudo, Yamato Suzuki, Noboru Itouyama, Ken Matsuoka, Koichi Matsuyama, Jiro Kasahara, Daisuke Nakata, Mio Namera, Hikaru Eguchi, Masaharu Uchiumi, Akiko Matsuo, Ikkoh Funaki, Shuichi Nakamura, Kazuyuki Higashino, Hidetoshi Hirashima，2024 AIAA SciTech，2024.01

  9. Operation Characteristics of Cylindrical Rotating Detonation Engine Using Liquid Ethanol and Liquid Nitrous Oxide

    Tomoki Sato, Kotaro Nakata, Satoru Sawada, Yamato Suzuki, Yusuke Kudo, Kosuke Nakajima, Noboru Itouyama, Ken Matsuoka, Jiro Kasahara, Akira Kawasaki, Mio Namera, Hikaru Eguchi, Daisuke Nakata, Masaharu Uchiumi, Akiko Matsuo, Ikkoh Funaki，2024 AIAA SciTech，2024.01

  10. The challenge of in-space demonstration of a cylindrical rotating detonation engine using liquid propellants by a sounding rocket S-520 launching,

    N. Itouyama, K. Ishihara, T. Sato, K. Nakata, K. Nakajima, K. Matsuyama, K. Matsuoka, A. Kawasaki, J. Kasahara, A. Matsuo, I. Funaki, D. Nakata, H. Eguchi, M. Uchiumi,，34th International Symposium on Space Technology and Science (ISTS)，2024.01

  11. Overview for the research and development of Rotating Detonation Engine Systems using a liquid-liquid propellant combination

    Noboru Itouyama, Koichi Matsuyama, Ken Matsuoka, Tomoki Sato, Kotaro Nakata, Satoru Sawada, Yusuke Kudo, Kosuke Nakajima, Yamato Suzuki, Jiro Kasahara, Akira Kawasaki, Mio Namera, Daisuke Nakata, Hikaru Eguchi, Masaharu Uchiumi, Akiko Matsuo, Ikkoh Funaki，2024 AIAA SciTech，2024.01

  12. A Bread Board Model Testing for In-Space Flight Demonstration of a Liquid-Propellant Detonation Engine System

    Akira Kawasaki, Kotaro Nakata,Tomoki Sato, Satoru Sawada, Yusuke Kudo, Yamato Suzuki, Noboru Itouyama, Ken Matsuoka, Koichi Matsuyama, Jiro Kasahara, Daisuke Nakata, Mio Namera, Hikaru Eguchi, Masaharu Uchiumi, Akiko Matsuo, Ikkoh Funaki, Shuichi Nakamura, Kazuyuki Higashino, Hidetoshi Hirashima，2024 AIAA SciTech，2024.01

  13. Experimental Study on propagation mode of Cylindrical Rotating Detonation Engine with Liquid Ethanol-Liquid Nitrous Oxide

    T. Sato, K. Ishihara, K. Nakata, T. Kimura, Y. Kikuchi, K. Nakajima, S. Sawada, M. Inada, R. Sakata, Y. Suzuki, Y. Oda, N. Itouyama, K. Matsuoka, J. Kasahara, A. Kawasaki, H. Watanabe, H. Okano, T. Tada, A. Fujiura, M. Namera, R.Nakazawa, H. Eguchi, D. Nakata, M. Uchiumi, A. Matsuo, I. Funaki，29th ICDERS，2023.07

  14. Experimental Study on propagation mode of Cylindrical Rotating Detonation Engine with Liquid Ethanol - Liquid Nitrous Oxide

    T. Sato, K. Ishihara, K. Nakata, T. Kimura, Y. Kikuchi, K. Nakajima, S. Sawada, M. Inada, R. Sakata, Y. Suzuki, Y. Oda, N. Itouyama, K. Matsuoka, J. Kasahara, A. Kawasaki, H. Watanabe, H. Okano, T. Tada, A. Fujiura, M. Namera, R.Nakazawa, H. Eguchi, D. Nakata, M. Uchiumi, A. Matsuo, I. Funaki，29th ICDERS，2023.07

  15. The challenge of in-space demonstration of a cylindrical rotating detonation engine using liquid propellants by a sounding rocket S-520 launching

    N. Itouyama, K. Ishihara, T. Sato, K. Nakata, K. Nakajima, K. Matsuyama, K. Matsuoka, A. Kawasaki, J. Kasahara, A. Matsuo, I. Funaki, D. Nakata, H. Eguchi, M. Uchiumi,，34th International Symposium on Space Technology and Science (ISTS)，2023.06

  16. Experimental Study on Thrust Performance of Cylindrical Rotating Detonation Rocket Engine with Liquid Ethanol - Liquid Nitrous Oxide

    Kazuki ISHIHARA, Tomoki SATO, Kotaro NAKATA, Tomoaki KIMURA, Kosuke NAKAJIMA, Yamato SUZUKI, Noboru ITOUYAMA, Ken MATSUOKA, Jiro KASAHARA, Akira KAWASAKI, Hikaru EGUCHI, Daisuke NAKATA, Masaharu UCHIUMI, Akiko MATSUO, Ikkoh FUNAKI, Hideto KAWASHIMA, and Makoto KOJIMA，The 11th Asian Joint Conference on Propulsion and Power，2023.03

  17. Numerical Estimation of Discharge Coefficient of Nitrous Oxide Flow inside an Injector for Hybrid Rocket Engine

    R. Watanabe, Y. Shimizu, K. Yasuda, and D. Nakata，33rd International Symposium on Space Technology and Science Proceedings，2022.02

  18. In-Space Flight Demonstration Results of a Detonation Engine System on 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, I. Funaki, D. Nakata, M. Uchiumi, H. Habu, S. Takeuchi, S. Arakawa, J. Masuda, K. Maehara, T. Nakao, K. Yamada，33rd International Symposium on Space Technology and Science Proceedings，2022.02

  19. In-Space Flight Demonstration Results of a Detonation Engine System on 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，33rd International Symposium on Space Technology and Science Proceedings，2022.02

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

    K. Goto, K. Matsuyama, K. Matsuoka, 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，33rd International Symposium on Space Technology and Science Proceedings，2022.02

  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

  41. Performance Characteristics of Low-Power Water-Cooled and Anode-Radiation-Cooled DC Arcjet Thrusters using Water and HAN Propellants with Special Vaporing Systems

    Hirokazu Tahara, Shunsuke Okumura, Kazuyoshi Okuda, Takefumi Mimura, Kyoko Takada, Ai Momozawa, Yuichiro Nogawa, Daisuke Nakata, Tomoyuki Ikeda，32nd International Symposium on Space Technology and Science，2019.06

  42. Development Progress of the Proof of Concept Hybrid Electro-Chemical Thruster

    Giulio Coral, Ryudo Tsukizaki, Kiyoshi Kinefuchi, Daisuke Nakata, Toru Shimada, Kazutaka Nishiyama, Hitoshi Kuninaka，32nd International Symposium on Space Technology and Science，2019.06

  43. Propulsive Performance of Rotating Detonation Engine with Methane for a Flight Demonstration on S-520-31

    Keisuke Goto, Ryuya Yokoo, Juhoe Kim, Akira Kawasaki, Ken Matsuoka, Jiro Kasahara, Akiko Matsuo, Ikkoh Funaki, Daisuke Nakata, Masaharu Uchiumi, Hideto Kawashima，32nd International Symposium on Space Technology and Science，2019.06

  44. Development Status of a Detonation Engine Testing Module Toward Flight Demonstration on S-520-31

    Akira Kawasaki, Jiro Kasahara, Ken Matsuoka, Keisuke Goto, Ryuya Yokoo, Ju-Hoe Kim, Akiko Matsuo, Ikkoh Funaki, Daisuke Nakata, Masaharu Uchiumi, Hiroto Habu, Shinsuke Takeuchi, Koki Kitagawa, Hirobumi Tobe, Kazuhiko Yamada, Asato Wada，32nd International Symposium on Space Technology and Science，2019.06

  45. Experimental Performance Validation of a Rotating Detonation Engine toward a Flight Demonstration

    Keisuke Goto, Ryuya Yokoo, Juhoe Kim, Akira Kawasaki, Ken Matsuoka, Jiro Kasahara, Akiko Matsuo, Ikkoh Funaki, Daisuke Nakata, Masaharu Uchiumi，AIAA Scitech Forum，2019.01

  46. Thermal Design and Experimental Verification of 3D-Printed Registojet

    Daisuke Nakata and Kiyoshi Kinefuchi，AIAA Propulsion and Energy Forum，2018.07

  47. 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，2018.07

  48. 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，2018.01

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

    Higashino, K.,Nakata, D. ,Minato, R.,Imai, R.,Tanatsugu, N.,Yashima, Y.,Mukae, H.，2017.09

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

    Minato, R.,Imai, R.,Higashino, K.,Nakata, D. ,Ishihara, M.，ISABE 2017 Conference，2017.09

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

    Nakata, D.,Yasuda, K.,Okada, K.,Higashino, K.,Watanabe, R.，31st International Symposium on Space Technology and Science，2017.06

  52. Research and Development of Rotating Detonation Engines for the Sounding Rocket Flight Experiment

    Kasahara, J.,Ishihara, K.,Nishimura, J.,Nakagami, S.,Matsuoka, K.,Matsuo A.,Funaki, I.,Mukae, H.,Yasuda, K.,Nakata, D.,Higashino, K.，The First International Constant Volume and Detonation Combustion Workshop，2017.06

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

    Iijima, A.,Nakata, D.,Higashino, K.，Propulsion and Energy Forum and Exposition 2016，2016.07

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

    Nakata, D.,Yasuda, K.,Horio, S.,Higashino, K.，Propulsion and Energy Forum and Exposition 2016，2016.07

  55. Development of a Small-scale Supersonic Flight Experiment Vehicle and its Prototype

    Nakata, D.，The 3rd Symposium on Flight Tests for the Innovative Aerospace Transportation Systems，2015.07

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

    Iijima, A.,Nakata, D.,Higashino, K.,Tanatsugu, N.,Ishimoto, S.,Azuma, N.，30th International Symposium on Space Technology and Science，2015.07

  57. Fundamental Study on Clustered Hybrid Rockets for Rocket Sled Propulsion System

    Nakata, D.,Horio, S.,Higashino, K.,Tanatsugu, N.，30th International Symposium on Space Technology and Science，2015.07

  58. Development of a Small-scale Supersonic Flight Experiment Vehicle as a Flying Test Bed

    Mizobata, K.,Minato, R.,Higuchi, K.,Ueba, M.,Takagi, S.,Nakata, D.,Katsumata, N.,Higashino, K.,Tanatsugu, N.，29th Congress of the International Council of the Aeronautical Sciences，2014.09

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

    Mizobata, K.,Minato, R.,Higuchi, K.,Ueba, M.,Takagi, S.,Nakata, D.,Higashino, K.,Tanatsugu, N.，The 29th International Symposium on Space Technology and Science，2013.06

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

    Nakata, D.,Tanatsugu, N.,Higashino, K.,Higuchi, K.,Tsuchiya, T.,Himeno,T.，Ground Based Space Facility Conference，2013

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