Výsledky vyhledávání - "プラズマコンタクタ"

Autor: Tahara, Hirokazu, Utsumi, Ryosuke

Publikováno v: 第27回宇宙エネルギーシンポジウム平成19年度 = The Twenty-seventh Space Energy Symposium. :68-72

ElectroDynamic Tether (EDT) is a long, thin conductive string deployed from a spacecraft. Traveling across the geomagnetic field and driving a current inside itself, EDT may be used to reboost/deboost a spacecraft to which EDT is attached. This is ma

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::91c87ad0d73719fac5d1cef82b1eb527
http://id.nii.ac.jp/1696/00008021/

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PIC simulation of spacecraft charging relaxation in arctic regions caused by active plasma discharge

Autor: Usui, Hideyuki, Imasato, Kojiro, Kuninaka, Hitoshi

Publikováno v: 宇宙航空研究開発機構特別資料: 第4回宇宙環境シンポジウム講演論文集 = JAXA Special Publication: Proceedings of the 4th Spacecraft Environment Symposium. :170-173

資料番号: AA0063997029
レポート番号: JAXA-SP-07-030

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::e10901d7d99eed7de3f212622e90edcb
http://id.nii.ac.jp/1696/00005512/

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JAXA/JEDI project on the development of plasma simulator for spacecraft environment

Autor: Usui, Hideyuki, Shinohara, Iku, Ueda Okada, Hiroko, Okada, Masaki

Publikováno v: 宇宙航空研究開発機構特別資料: 宇宙航空研究開発機構情報・計算工学センター衛星環境プラズマ数値シミュレーションワークショップ報告書 = JAXA Special Publication: JAXA/JEDI Workshop on Numerical Plasma Simulation for Spacecraft Environment. :28-34

2005年度にJAXA情報・計算工学センター(JEDI; JAXA's Engineering Digital Innovation Center)が発足し、これまで行われた宇宙プラズマ物理解析のプラズマシミュレーションを衛星機器の技術開発、衛星�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::8e92dc86992abee6520233e3f276c87e
http://id.nii.ac.jp/1696/00005903/

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Analysis of three dimensional motion of an electrodynamic tether system on elliptical orbits

Autor: Kishimoto, Tomoko, Yamagiwa, Yoshiki

Publikováno v: 宇宙輸送シンポジウム平成15年度 = Proceedings of Space Transportation Symposium FY2003. :292-295

資料番号: AA0047118072

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::43a1f20e2c7c8534d209509deef3e830
http://id.nii.ac.jp/1696/00017296/

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宇宙機表面のアーキングに関する地上実験と数値計算

Autor: Tahara, Hirokazu, Masuyama, Takahisa

Publikováno v: 宇宙航空研究開発機構特別資料: 宇宙インフラストラクチャ研究会宇宙環境計測技術WG:第6回宇宙飛翔体環境研究会報告書 = JAXA Special Publication: Proceedings of the 6th Spacecraft Environment Research Network Meeting. :37-42

In the future, LEO spacecraft will be larger and higher powered. Because of the balance of leakage currents through ambient space plasma, their main conductive body will have a higher negative potential without plasma contactor operation. When spacec

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::4f6fd034e2d6413a8cfc74863b31db4d
http://id.nii.ac.jp/1696/00006646/

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Study on ground-based experiments of a plasma contactor

Autor: Kosakai, Masaya, Takegahara, Haruki

Publikováno v: 宇宙輸送シンポジウム平成13年度 = Proceedings of Space Transportation Symposium FY2001. :201-204

ホローカソードプラズマコンタクタに対して、電子を放出するエミッタと電子を収集するコレクタをプラズマ環境下で同時作動させることにより、エレクトロダイナミックテザーの電流�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::c0e32b49a3b0ed6a8beb293225eba047
http://id.nii.ac.jp/1696/00017472/

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