Rchr
J-GLOBAL ID:201901000103495879   Update date: Jul. 17, 2024

Kawashima Rei

カワシマ レイ | Kawashima Rei
Affiliation and department:
Job title: Associate Professor
Homepage URL  (2): https://www.sepl.ee.shibaura-it.ac.jp/https://sites.google.com/shibaura-it.ac.jp/sepl-en
Research field  (1): Aerospace engineering
Research theme for competitive and other funds  (11):
  • 2024 - 2028 高密度イオン推進機における乱れの付加を利用した電子輸送の促進と抑制
  • 2024 - 2027 Satellite orbit control utilizing charging phenomena resulting from differences in ion-electron magnetization induced by satellite magnetic fields
  • 2023 - 2026 Development of an Ablative Propellant Hall Thruster
  • 2024 - 2024 Structure-Preserving Numerical Method for Anisotropic Diffusion Problems in Rarefied Plasmas
  • 2021 - 2024 宇宙プラズマと衛星磁場のイオンスケール相互作用の解明に基づく軌道維持機能の創出
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Papers (44):
  • Ayuto Manabe, Hanco Britz, François Gutierrez, Aida van de Wetering, Tatsuki Kinoshita, Kimiya Komurasaki, Rei Kawashima, Hokuto Sekine, Hiroyuki Koizumi. Numerical Analysis on Multi-Cycle Operation of Microwave Rocket with Reed Valve Air-Breathing System. JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 2024. 72. 2. 29-40
  • Kuniyoshi Tabata, Yasuhisa Oda, Kimiya Komurasaki, Ayuto Manabe, Rei Kawashima. Non-equilibrium aerodynamics between ionization-wave and shock-wave fronts in millimetre-wave supported detonation. Japanese Journal of Applied Physics. 2023. 62. 11. 116001
  • R Kawashima. Sheath Analysis of Conducting Channel Walls in Anode-Layer Hall Thruster with Acceleration Zone Shifted Downstream. Frontier of Applied Plasma Technology. 2023. 16. 1
  • Dibyesh Satpathy, Shu Kawabata, Hokuto Sekine, Rei Kawashima, Kimiya Komurasaki, Hiroyuki Koizumi. Investigation of correlation between thrust and anode temperature during transient operation of RAIJIN-66. Journal of Electric Propulsion. 2023. 2. 1
  • Kuniyoshi Tabata, Ayuto Manabe, Yoshiki Takase, Kimiya Komurasaki, Rei Kawashima, Hokuto Sekine. Plasma Structure and Non-Equilibrium Thermodynamics of Atmospheric Millimeter-Wave Discharge in Microwave Rocket. AIAA AVIATION 2022 Forum. 2022
more...
MISC (65):
  • R. Kawashima, K. Komurasaki. Numerical Analysis of the Gradient Drift Instability and its Control in Hall Thruster Plasmas. AAPPS-DPP2023. 2023
  • R. Kawashima. Extracting Electron Transport Property Enhanced by Gradient Drift Instability in Hall Thruster. Plasma Application and Hybrid Functionally Materials. 2023
  • J. Bak, R. Kawashima, K. Komurasaki. Plasma formation and electron cross-field transport in the axial-azimuthal plane of a Hall thruster. 37th International Electric Propulsion Conference. 2022
  • R. Kawashima. Numerical and Experimental Simulations of Magnetic Plasma Orbit Control for Nanosatellites. Plasma Application and Hybrid Functionally Materials. 2022
  • R. Kawashima, K. Komurasaki. Hybrid-PIC Simulation of Gradient Drift Instabilities in Hall Thrusters for Electron Transport Analysis. 37th International Electric Propulsion Conference. 2022
more...
Professional career (1):
  • 博士(工学) (東京大学)
Awards (4):
  • 2022/04 - Encouragement Award Nano-satellite Formation Keeping Using Magnetic Torquer-induced Differential Plasma Force
  • 2022/03 - 航空原動機・宇宙推進講演会 若手優秀講演賞 ホールスラスタ性能予測へ向けた勾配ドリフト不安定性の数値シミュレーション
  • 2019/03 - Best Paper Award Hybrid PIC Simulation of a Thruster with Anode Layer with Self-Consistent Electron Transport Model
  • 2014/04 - 日本航空宇宙学会年会講演会 学生優秀発表賞 双曲型方程式系による準中性プラズマ中電子流体計算
Association Membership(s) (3):
Institute of Applied Plasma Science ,  AIAA ,  日本航空宇宙学会
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