CiNii Articles - Hall thruster

1

Electron extraction enhancement via the magnetic field in a miniature microwave discharge neutralizer

Sato Yosuke , Koizumi Hiroyuki , Nakano Masakatsu , Takao Yoshinori

This study analyzes the dependence of electron extraction efficiency, which is defined as the ratio of the extracted electron current to the generated electron current, on the orifice shapes and magne …

Journal of Applied Physics 126(24), 243302, 2019-12-23

IR
2

Status Report on the R&Ds of Japanese 6-kW-class Hall Thrusters [in Japanese]

船木一幸 , 張科寅 , 佐野伊彦 , 深津敦 , 田代洋輔 , 椎木泰三

年会講演会講演集 50, 4p, 2019-04-18
3

Numerical Analysis on the Plasma Behavior of a Hydrogen MPD Thruster at the Critical Current [in Japanese]

Tauchi Shitan , Kawasaki Akira , Nakane Masakatsu , Kubota Kenichi , Funaki Ikkoh

… For a self-field magnetoplasmadynamic (MPD) thruster using hydrogen propellant, plasma flows were numerically simulated with a model including the ion-slip effect. … To clarify the thruster behavior near the critical current, the discharge current and the propellant mass flow rate were set to 5 or 10 kA (critical current) and 0.4 g/s, respectively. …

JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 67(5), 159-166, 2019

J-STAGE
4

1,000-hours Demonstration of a 6-kW-class Hall Thruster for All-Electric Propulsion Satellite

FUNAKI Ikkoh , MATSUNAGA Yoshiki , FUCHIGAMI Kenji , CHO Shinatora , SANO Tadahiko , FUKATSU Tsutomu , TASHIRO Yosuke , SHIIKI Taizo , NAKAMURA Yoichiro , WATANABE Hiroki , KUBOTA Kenichi

… A 1,000-hours preliminary life test of a 6-kW-class xenon Hall thruster for Engineering Test Satellite-9 (ETS-9) was conducted by using a bread board model thruster. … The thruster was disassembled at an accumulated operational time of 652 hours to find 2.3-mm erosion at the channel's downstream surfaces. …

TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN 17(5), 589-595, 2019

J-STAGE
5

Experimental Investigation of LaB6 Hollow Cathode with Radiative Heater

OSHIO Yuya , KUBOTA Kenichi , WATANABE Hiroki , CHO Shinatora , OHKAWA Yasushi , FUNAKI Ikkoh

… A lanthanum hexaboride (LaB6) hollow cathode with radiative heater has been developed for high power Hall thruster neutralizer. …

TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN 17(2), 203-210, 2019

J-STAGE
6

Research and Development of Cylindrical Hall Thrusters for Powered Flight of Micro/Nano Moon Exploration Satellite 3rd PROITERES at Osaka Institute of Technology [in Japanese]

TAHARA Hirokazu , KOBAYASHI Mitsuyoshi , KAWAKAMI Tensei , TAGAWA Masumi , TAKADA Kyoko , IKEDA Tomoyuki

… を行っており，超小型月探査衛星プロイテレス衛星3号機の計画を立案している．月探査を達成するには推進機による軌道遷移が必要である．そこで，シリンドリカル型ホールスラスタ（Cylindrical Hall Thruster : CHT）に着目し，開発を行ってきた．50kgの超小型人工衛星に推進剤を15～20kg搭載したとすると，比推力が1,300～1,900s必要である．そこで投入電力50W程度，比推力1,300s以上を推進機の目標性能とし …

Aeronautical and Space Sciences Japan 67(2), 53-58, 2019

J-STAGE
7

ホールスラスタ内部解析用PIC法計算のArria 10 SoC FPGAへの実装 (回路とシステム) [in Japanese]

野田裕之 , 宮島敬明 , 藤田直行 , 天野英晴

電子情報通信学会技術研究報告 = IEICE technical report : 信学技報 118(373), 119-124, 2018-12-21
8

ホールスラスタ内部解析用PIC法計算のArria 10 SoC FPGAへの実装 (集積回路) [in Japanese]

野田裕之 , 宮島敬明 , 藤田直行 , 天野英晴

電子情報通信学会技術研究報告 = IEICE technical report : 信学技報 118(374), 119-124, 2018-12-21
9

Progress of Theory and Simulation on Ionization Oscillations in Hall Effect Thrusters [in Japanese]

原健太郎

プラズマ・核融合学会誌 = Journal of plasma and fusion research 94(10), 475-481, 2018-10
10

Distributions of Plasma Parameters in a Hall Thruster with Non-uniform Propellant Supply in Azimuth [in Japanese]

朴俊輝 , 川嶋嶺 , 小紫公也 , 小泉宏之

年会講演会講演集 49, 6p, 2018-04-19
11

Electrostatic Thrusters [in Japanese]

山本直嗣 , 渡邊裕樹

プラズマ・核融合学会誌 = Journal of plasma and fusion research 94(2), 71-75, 2018-02
12

Current and Future Missions Using Electric Rocket Propulsion [in Japanese]

西山和孝 , 杵淵紀世志

プラズマ・核融合学会誌 = Journal of plasma and fusion research 94(2), 60-65, 2018-02
13

Status Report on the Development of a Hall Thruster for Japanese All-Electric Propulsion Satellite [in Japanese]

FUNAKI Ikkoh , CHO Shinatora , SANO Tadahiko , FUKATSU Tsutomu , TASHIRO Yosuke , SHIIKI Taizo , NAKAMURA Yoichiro

3～6トンの中型から大型の静止衛星市場では，衛星推進系を電気推進にて運用する「オール電化衛星」の利用が急速に拡大しつつある．宇宙航空研究開発機構（JAXA）技術試験衛星9号機（ETS9）プロジェクトチームでは，大型衛星の軌道遷移と軌道保持の双方に利用可能な大型ホールスラスタシステムの開発を実施している．本稿では，ETS9搭載ホールスラスタの開発状況について報告する．最新のブレッド …

Aeronautical and Space Sciences Japan 66(11), 346-351, 2018

J-STAGE
14

Prediction of Discharge Current using Neural Network in Hall Thruster [in Japanese]

Fuchigami Hirotaka , Chono Masatoshi , Yamamoto Naoji

… We have been developing a prediction code of discharge current using neural network for constructing auto-controlling system in Hall thrusters. …

JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 66(5), 143-145, 2018

J-STAGE
15

Development of a Numerical Tool for Hall Thruster Plume and Spacecraft Interaction Analysis

MURANAKA Takanobu , INANAGA Yasutaka

… A three-dimensional electrostatic numerical tool has been developed to analyze spacecraft and Hall thruster plume interactions to evaluate spacecraft reliability under operation of the thruster in its designing phase. …

TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN 16(5), 366-373, 2018

J-STAGE
16

Numerical Sensitivity Analysis of Chamber Backpressure Effect in Hall Thruster Experiment [in Japanese]

Cho Shinatora , Watanabe Hiroki , Kubota Kenichi , Funaki Ikkoh

… Facility backpressure effect remains to be an important unsolved problem for Hall thruster development making it difficult to predict the thruster on-orbit operation precisely. … 10% increment of thrust and current can be observed even if the recommended pressure criteria for Hall thruster measurement is satisfied. …

JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 66(3), 61-68, 2018

J-STAGE
17

Experimental test of 200 W Hall thruster with titanium wall

Ding Yongjie , Sun Hezhi , Peng Wuji , Xu Yu , Wei Liqiu , Li Hong , Li Peng , Su Hongbo , Yu Daren

Japanese Journal of Applied Physics 56(5), 050312-050312, 2017-04-21

DOI
18

R&D of Hall Thrusters for All-electric Propulsion Satellite [in Japanese]

船木一幸 , 飯原重保 , 張科寅 , 窪田健一 , 渡邊裕樹 , 渕上健児 , 伊藤彦 , 田代洋輔

年会講演会講演集 48, 4p, 2017-04-13
19

Measurement of Hall thruster UT58 plume divergence in the vicinity of channel outlet [in Japanese]

水川将暢 , 朴俊輝 , 濱田悠嗣 , 川嶋嶺 , 小紫公也 , 小泉宏之 , 小林鶴雄

年会講演会講演集 48, 5p, 2017-04-13
20

Numerical Analysis on the Rotating Spoke Phenomenon in Hall Thrusters [in Japanese]

川嶋嶺 , 朴俊輝 , 小紫公也 , 小泉宏之

年会講演会講演集 48, 6p, 2017-04-13

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