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Research on plasma analysis method in electric propulsion

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JAXA Supercomputer System Annual Report February 2024-January 2025 Report Number: R24ECWU04 Subject Category: Cooperative Graduate School System PDF Responsible Representative: Yasuhiro Mizobuchi, Aviation Technology Directorate, XANADU Project Team Contact Information: Kiyoshi Kinefuchi, Department of Aerospace Engineering, Graduate School of Engineering, Nagoya University(kiyoshi.kinefuchi@mae.nagoya-u.ac.jp) Members: Satoshi Inoue, Masaya Ikuta, Ryohei Takagi Abstract The objective of this study is to understand plasma physics phenomena in electric propulsion systems such as hollow cathode and MPD thruster. In order to investigate the distribution of plasma・・・<<read more>>

Study on spacecraft dynamics

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JAXA Supercomputer System Annual Report February 2024-January 2025 Report Number: R24ECWU24 Subject Category: Cooperative Graduate School System PDF Responsible Representative: Yusuke Maru, Associate Professor, Institute of Space and Astronautical Science Contact Information: Yusuke Maru(maru.yusuke@jaxa.jp) Members: Hiroto Aoyagi, Shoya Koshino, Ryota Miyajima, Kazuma Matsumoto, Yuma Miki, Takumi Ohno, Keisuke Takahashi, Daiki Watanabe, Tsubasa Watabe, Maiko Yamakawa Abstract Specifically, we performed (1) a performance analysis of the air intake of an air-breathing engine installed on a space transport aircraft, (2) an evaluation・・・<<read more>>

Gas-Liquid Two Phase Flow Behavior Related to ECLSS

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JAXA Supercomputer System Annual Report February 2024-January 2025 Report Number: R24ECWU77 Subject Category: Cooperative Graduate School System PDF Responsible Representative: Masato Sakurai, Manager of ECLSS, Research Unit II, Aerospace RInsertHereD Directorate, JAXA Contact Information: Masato Sakurai(sakurai.masato@jaxa.jp) Members: Hikono Furuichi, Motoharu Kusano, Gaku Murakami, Masato Sakurai Abstract Elucidate the effects of gravity on gas-liquid two-phase flows to develop separation techniques for gas-liquid two-phase flows generated by the operation of the Environment Control and Life Support System (ECLSS). Reference URL N/A Reasons・・・<<read more>>

Acoustic Liner Program for future High-bypass-ratio Aircraft engines(Development of combustor)

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JAXA Supercomputer System Annual Report February 2024-January 2025 Report Number: R24EDA101C39 Subject Category: Aeronautical Technology PDF Responsible Representative: Kenichiro Nagai, Aeronautical Technology Directorate,Aviation Environmental Sustainability Innovation Contact Information: Naoyuki Okamura(okamura.naoyuki@jaxa.jp) Members: Taisuke Nambu, Hideji Saiki Abstract In this project, we will apply next-generation acoustic liner to combustor. To perform the numerical analysis of combustor with the acoustic liner by using HINOCA-AE which is CFD solver for aircraft engine combustors. Reference URL N/A Reasons and benefits of using JAXA Supercomputer System・・・<<read more>>

Acoustic Liner Program for High-bypass-ratio Aircraft engines (acoustic performance improvement)

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JAXA Supercomputer System Annual Report February 2024-January 2025 Report Number: R24EDA101C75 Subject Category: Aeronautical Technology PDF Responsible Representative: Kenichiro Nagai, Aeronautical Technology Directorate, Aviation Environmental Sustainability Innovation Hub Contact Information: Shunji ENOMOTO(enomoto.shunji@jaxa.jp) Members: Shunji Enomoto Abstract Ultra high bypass ratio aviation jet engines have a smaller sound absorbing liner area than conventional engines. In this project, we will develop sound-absorbing device technology that provides high noise reduction performance even with a small-sized sound-absorbing liner. Reference URL N/A Reasons and benefits・・・<<read more>>