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Rei KAWASHIMA
Rei KAWASHIMA
Unknown affiliation
Verified email at shibaura-it.ac.jp
Title
Cited by
Cited by
Year
Numerical analysis of azimuthal rotating spokes in a crossed-field discharge plasma
R Kawashima, K Hara, K Komurasaki
Plasma Sources Science and Technology 27 (3), 035010, 2018
572018
Hall thruster development for Japanese space propulsion programs
Y Hamada, J Bak, R Kawashima, H Koizumi, K Komurasaki, N Yamamoto, ...
Transactions of the japan society for aeronautical and space sciences 60 (5 …, 2017
362017
Magnetic plasma deorbit system for nano-and micro-satellites using magnetic torquer interference with space plasma in low Earth orbit
T Inamori, R Kawashima, P Saisutjarit, N Sako, H Ohsaki
Acta astronautica 112, 192-199, 2015
362015
Operating parameters and oscillation characteristics of an anode-layer Hall thruster with argon propellant
D Fujita, R Kawashima, Y Ito, S Akagi, J Suzuki, T Schönherr, H Koizumi, ...
Vacuum 110, 159-164, 2014
252014
Particle simulation of plasma drag force generation in the magnetic plasma deorbit
R Kawashima, J Bak, S Matsuzawa, T Inamori
Journal of Spacecraft and Rockets 55 (5), 1074-1082, 2018
202018
A hyperbolic-equation system approach for magnetized electron fluids in quasi-neutral plasmas
R Kawashima, K Komurasaki, T Schönherr
Journal of Computational Physics 284, 59-69, 2015
202015
Plasma formation and cross-field electron transport induced by azimuthal neutral inhomogeneity in an anode layer Hall thruster
J Bak, R Kawashima, K Komurasaki, H Koizumi
Physics of Plasmas 26 (7), 2019
182019
Alumina reduction by laser ablation using a continuous-wave CO2 laser toward lunar resource utilization
S Tanaka, S Yamada, R Soga, K Komurasaki, R Kawashima, H Koizumi
Vacuum 167, 495-499, 2019
172019
Effect of capacitance on discharge behavior of pulsed plasma thruster
T SCHÖNHERR, K Komurasaki, R Kawashima, Y ARAKAWA, ...
Journal of IAPS プラズマ応用科学 Vol 18 (1), 2010
132010
High-order upwind and non-oscillatory approach for steady state diffusion, advection–diffusion and application to magnetized electrons
AS Chamarthi, K Komurasaki, R Kawashima
Journal of Computational Physics 374, 1120-1151, 2018
122018
Two-dimensional hybrid model of gradient drift instability and enhanced electron transport in a Hall thruster
R Kawashima, K Komurasaki
Physics of Plasmas 28 (6), 2021
112021
Characterization of acceleration zone shifting in an anode-layer-type Hall thruster RAIJIN66
Y Hamada, R Kawashima, J Bak, K Komurasaki, H Koizumi
Vacuum 186, 110040, 2021
102021
Effects of azimuthal non-uniformity on the Hall thruster discharge
R Kawashima, J Bak, K Komurasaki, H Koizumi, K Hara
The 35th International Electric Propulsion Conference 527, 2017, 2017
102017
A flux-splitting method for hyperbolic-equation system of magnetized electron fluids in quasi-neutral plasmas
R Kawashima, K Komurasaki, T Schönherr
Journal of Computational Physics 310, 202-212, 2016
102016
Novel ideas for nanosatellite constellation missions
R Sandau, S Nakasuka, R Kawashima, JJ Sellers
(No Title), 2012
92012
Discharge characteristics and increased electron current during azimuthally nonuniform propellant supply in an anode layer Hall thruster
J Bak, B Van Loo, R Kawashima, K Komurasaki
Journal of Applied Physics 128 (2), 2020
82020
Characterization of reduction products generated by laser ablation of alumina
S Yamada, S Tanaka, K Komurasaki, R Kawashima, H Koizumi
Journal of IAPS 26 (1), 33-38, 2018
82018
Evaluation of discharge behavior of the pulsed plasma thruster SIMP-LEX
T Schönherr, K Komurasaki, R Kawashima, Y Arakawa, G Herdrich
46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 6530, 2010
82010
Plasma structure and electron cross-field transport induced by azimuthal manipulation of the radial magnetic field in a Hall thruster E× B discharge
J Bak, R Kawashima, G Romanelli, K Komurasaki
Journal of Applied Physics 131 (5), 2022
72022
Development status of 5 kw class anode-layer type Hall thruster: RAIJIN94
Y Hamada, R Kawashima, K Komurasaki, N Yamamoto, H Tahara, ...
International Electric Propulsion Conference, IEPC-2017-412, 2017
62017
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