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 | 57 | 2018 |

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 | 36 | 2017 |

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 | 36 | 2015 |

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 | 25 | 2014 |

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 | 20 | 2018 |

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 | 20 | 2015 |

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 | 18 | 2019 |

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 | 17 | 2019 |

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 | 13 | 2010 |

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 | 12 | 2018 |

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 | 11 | 2021 |

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 | 10 | 2021 |

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 | 10 | 2017 |

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 | 10 | 2016 |

Novel ideas for nanosatellite constellation missions R Sandau, S Nakasuka, R Kawashima, JJ Sellers (No Title), 2012 | 9 | 2012 |

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 | 8 | 2020 |

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 | 8 | 2018 |

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 | 8 | 2010 |

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 | 7 | 2022 |

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 | 6 | 2017 |