International conference proceedings - Nakata Daisuke

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