Rchr
J-GLOBAL ID:201901000103495879
Update date: Mar. 15, 2025
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 (12):
- 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
- 2025 - 2025 Mathematical Model and Numerical Methods for Understanding Instability Phenomena in Rarefied Plasmas
- 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
- 2020 - 2024 Digital Twin Creation of High-Density Ion Thruster with Electron Anomalous Transport Control
- 2023 - 2023 Mathematical Model and Numerical Schemes for Industrial Applications of Rarefied Plasma Analysis
- 2021 - 2023 アブレーション推進剤を持つイオン推進機の開発
- 2017 - 2020 Hall Thruster Discharge Stabilization by Artificial Disturbances
- 2015 - 2018 Formation flight using plasma drag force generated by an electromagnetic coil for small satellites
- 2012 - 2015 液体推進剤パルス型プラズマスラスタにおけるプラズマの発生及び加速過程の解明
Show all
Papers (50):
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Junhwi Bak, Rei Kawashima. Is anomalous electron cross-field transport always detrimental?: potential applications of deliberately enhanced transport in Hall thrusters. Journal of Electric Propulsion. 2025. 4. 1
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Dibyesh SATPATHY, Hokuto SEKINE, Nadine BARTH, Rei KAWASHIMA, Kimiya KOMURASAKI, Hiroyuki KOIZUMI. Experimental Investigation on Ionization Length Required for Efficient Operation of Argon Hall Thrusters. TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 2025. 68. 1. 12-18
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Dibyesh Satpathy, Hokuto Sekine, Jiwon Lee, Kimiya Komurasaki, Rei Kawashima, Hiroyuki Koizumi. Influence of propellant injection directionality on the performance of an argon Hall thruster. Journal of Applied Physics. 2024
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Ryo Kameyama, Rei Kawashima, Takaya Inamori. Effects of Satellite Body on Magnetic Plasma Orbit Control for Nanosatellites. Frontier of Applied Plasma Technology. 2024. 17. 38-41
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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
more...
Lectures and oral presentations (70):
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Drag Force Augmentation of Magnetic Plasma Deorbit Method for Nanosatellites
(31st Annual Meeting of IAPS 2024)
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Electron Transport Enhancement by Artificial Disturbance in Near-Anode Region of Hall Thruster
(31st Annual Meeting of IAPS 2024)
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Control of Gradient Drift Instability and Electron Transport by Artificial Disturbances in Hall Thrusters
(38th International Electric Propulsion Conference 2024)
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Is anomalous electron cross-field transport always detrimental?: Potential applications of deliberately enhanced transport in Hall thrusters
(38th International Electric Propulsion Conference 2024)
-
Propellant Utilization Efficiency of an Argon Hall thruster with Swirl Injection
(38th International Electric Propulsion Conference 2024)
more...
Professional career (1):
Awards (5):
- 2022/04 - Encouragement Award Nano-satellite Formation Keeping Using Magnetic Torquer-induced Differential Plasma Force
- 2022/03 - 第61回航空原動機・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
- 2015/07 - ISTS/IEPC/NSAT Joint Conference Best Poster Award First Prize
- 2014/04 - 日本航空宇宙学会第45期年会講演会 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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