Xiang Ma, Yuya Oshio, Takeru Furukawa, Hiroyuki Nishida. Numerical investigation of antenna position effect on thrust of a radio-frequency plasma thruster with a magnetic cusp. Physics of Plasmas. 2025. 32. 9. 093501-1-093501-17
Takeru Furukawa, Daisuke Kuwahara, Shunjiro Shinohara. Ion flow velocimetry with Ar-II laser-induced fluorescence method in the rotating magnetic field plasma acceleration under a diverging magnetic field. Physics of Plasmas. 2025. 32. 7. 073512
Takeru Furukawa, Daisuke Kuwahara, Shunjiro Shinohara. Dependence of plasma dynamics on the strength of spatiotemporal-changing magnetic field in an RF plasma thruster using rotating magnetic field acceleration method. Plasma Sources Science and Technology. 2024. 33. 12. 125010-125010
Takeru Furukawa, Kento Shimasaki, Satoshi Nakamoto, Hiromasa Takeno. Influence of cusp-shaped magnetic fields on plasma density and thrust in an RF plasma thruster with a magnetic nozzle. Physics of Plasmas. 2024. 31. 11
Takumi Seto, Naomichi Ezumi, Reina Miyauchi, Takuma Okamoto, Satoshi Takahashi, Kosuke Takanashi, Keishi Kouno, Hiroto Kawahara, Mafumi Hirata, Junko Kohagura, et al. Effect of the magnetic field strength on the argon plasma characteristics of a helicon plasma source with a two-turn flat-loop antenna. Journal of Plasma Physics. 2024. 90. 4
A basic study of grid-less electrode application to traveling wave direct energy converter
(14th International Conference on Open Magnetic Systems for Plasma Confinement 2025)
Influence on plasma flow using rotating magnetic field plasma acceleration in a miniature RF plasma thruster
(14th International Conference on Open Magnetic Systems for Plasma Confinement 2025)
Plasma characteristics and acceleration in a miniature radio frequency plasma thruster using rotating magnetic field
(39th International Electric Propulsion Conference (IEPC) 2025)
Dependence of Plasma Profile on External Magnetic Field Condition in RF Plasma Thruster with a Magnetic Cusp
(35th ISTS & 14th NSAT 2025)
Evaluation of plasma acceleration effect in a small magnetic nozzle-type thruster using the rotating magnetic field method
(35th ISTS & 14th NSAT 2025)