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Dive into the research topics where Yuichi Nakagawa is active.

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Featured researches published by Yuichi Nakagawa.


Japanese Journal of Applied Physics | 2016

Electron extraction mechanisms of a micro-ECR neutralizer

Yoshinori Takao; Kenta Hiramoto; Yuichi Nakagawa; Yusuke Kasagi; Hiroyuki Koizumi; Kimiya Komurasaki

Three-dimensional particle simulations have been conducted to analyze the mechanisms of electron extraction through the orifices of a 4.2 GHz microwave discharge microneutralizer, using a xenon electron cyclotron resonance plasma. The dimensions of the neutralizer are 20 × 20 × 4 mm3, and a ring-shaped microwave antenna and permanent magnets are employed for its discharges. The numerical model is composed of a particle-in-cell simulation with a Monte Carlo collision algorithm for charged particle motions, a finite-difference time-domain method for microwaves, and a finite element analysis for magnetostatic fields. The simulation results have shown that the electrostatic field inside the plasma source has a dominant effect on electron extraction. The extracted electrons move along the magnetic field line to the orifice entrances and the E × B drift at the orifice edge induces electron extraction.


Physics of Plasmas | 2017

Effects of E × B drift on electron transport across the magnetic field in a miniature microwave discharge neutralizer

Kenta Hiramoto; Yuichi Nakagawa; Hiroyuki Koizumi; Yoshinori Takao

Using a three-dimensional particle-in-cell model, electron transport across a magnetic field has been investigated by obtaining the time-varying electric field and plasma parameters in a miniature microwave discharge neutralizer. The size of the neutralizer is 20 × 20 × 4 mm3. Ring-shaped antenna producing 4.2 GHz microwaves and permanent magnets for xenon plasma discharges are present inside. There are four orifices for electron extraction. The simulation area consists of both the discharge chamber and the vacuum region for the extraction. The numerical results show that radial striped patterns occur where the peak electron density is obtained, and the patterns seem to rotate in the azimuthal direction. This characteristic structure is very similar to recent results obtained in Hall thrusters and is probably due to the electron drift instability. Owing to the plasma structure, the azimuthal electric field is generated, which results in the E × B drift velocity in the axial direction with the radial magne...


Physics of Plasmas | 2018

Numerical simulation of full-aperture-pair ion optics in a miniature ion thruster

Masakatsu Nakano; Kengo Nakamura; Yuichi Nakagawa; D. Tomita; Yoshinori Takao; Hiroyuki Koizumi

The 211-aperture-pair two-grid ion optics of a miniature ion thruster is numerically simulated. Since the plasma in the miniature ion thruster is too inhomogeneous to introduce mirror or translational boundary conditions between apertures, all the apertures of the grid system are considered. The simulation is self-consistent, the ion current profile in the discharge chamber plasma is given by the particle-in-cell with Monte Carlo collision algorithm calculations, and all the ion beams extracted from the full-aperture-pair array were tracked including charge-exchange ions. A scheme for the construction of the full-aperture-pair simulation domain is proposed based on the array of a six-fold hexagonal single-aperture-pair simulation domain, which can be extended to other numbers of aperture pairs. Numerical results on accel impingement current and ion-beam profile are compared to experimental data and shown to be in reasonable agreement. Furthermore, the full-aperture-pair ion-optics model is compared with t...


Transactions of The Japan Society for Aeronautical and Space Sciences, Space Technology Japan | 2016

Initial Flight Operations of the Miniature Propulsion System Installed on Small Space Probe: PROCYON

Hiroyuki Koizumi; Hiroki Kawahara; Kazuya Yaginuma; Jun Asakawa; Yuichi Nakagawa; Yusuke Nakamura; Shunichi Kojima; Toshihiro Matsuguma; Ryu Funase; Junichi Nakatsuka; Kimiya Komurasaki


Archive | 2015

On-orbit Performance of a Miniature Propulsion System on a 70 kg Space Probe to Explore Near-Earth Asteroids

Hiroyuki Koizumi; Hiroki Kawahara; Kazuya Yaginuma; Jun Asakawa; Yuichi Nakagawa; Junichi Nakatsuka; Satoshi Ikari; Ryu Funase; Kimiya Komurasaki


Journal of The Japan Society for Aeronautical and Space Sciences | 2016

Thrust Vector Management of Electric Propulsion System for Micro-Spacecraft and Its On-Orbit Validation Results

Kazuya Yaginuma; Hiroyuki Koizumi; Hiroki Kawahara; Jun Asakawa; Yuichi Nakagawa; Tadashi Inagaki; Yusuke Kasagi; Satoshi Ikari; Naoya Ozaki; Ryu Funase; Kimiya Komurasaki


Transactions of The Japan Society for Aeronautical and Space Sciences | 2018

Numerical Analysis of a Miniature Microwave-discharge Ion Thruster Using Water as the Propellant

Kengo Nakamura; Yuichi Nakagawa; Hiroyuki Koizumi; Yoshinori Takao


Archive | 2016

Micropropulsion Systems Enabling Full Active Debris Removal by a Small Satellite ADRAS-1

Hiroyuki Koizumi; Jun Asakawa; Yuichi Nakagawa; Shunichi Kojima; Hiroki Kawahara; Kimiya Komurasaki; Masakatsu Nakano; Hinori Sahara; Mayu Banno; Jun Matsushima; Masahiro Kaku; Toshiaki Iizuka; Yuki Seto


Bulletin of the American Physical Society | 2016

Electron drift across the magnetic field in a micro-ECR neutralizer

Yoshinori Takao; Kenta Hiramoto; Yuichi Nakagawa; Hiroyuki Koizumi; Kimiya Komurasaki


52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016 | 2016

3D particle simulation for electron extraction mechanisms of a miniature microwave discharge neutralizer

Kenta Hiramoto; Yuichi Nakagawa; Hiroyuki Koizumi; Kimiya Komurasaki; Yoshinori Takao

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Yoshinori Takao

Yokohama National University

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Kenta Hiramoto

Yokohama National University

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Junichi Nakatsuka

Japan Aerospace Exploration Agency

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