Výsledky vyhledávání - "Nishida, Michio"

Dissertation/ Thesis

Novel humanized anti-CD20 monoclonal antibodies with unique germline VH and VL gene recruitment and potent effector functions

Autor: Nishida, Michio

Kyoto University (京都大学)
0048
乙第12264号
論医博第1966号
新制||医||971(附属図書館)
UT51-2008-N528
学位規則第4条第2項該当

Externí odkaz: http://hdl.handle.net/2433/124332

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Dissertation/ Thesis

STUDIES ON SHOCK-WAVE STRUCTURE IN A NONEQUILIBRIUM, PARTIALLY IONIZED GAS FLOW

Autor: Nishida, Michio

Kyoto University (京都大学)
0048
甲第938号
工博第180号
新制||工||142(附属図書館)
2354
UT51-45-Q43
学位規則第5条第1項該当

Externí odkaz: http://hdl.handle.net/2433/213239

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低エネルギーXe原子による炭素スパッタリングのデータベース構築

Autor: Muramoto, Tetsuya, Hyakutake, Toru, Nishida, Michio, Kenmotsu, Takahiro

Publikováno v: 宇宙輸送シンポジウム: 講演集録 = Proceedings of Space Transportation Symposium. :1-10

平成20年度宇宙輸送シンポジウム(2009年1月19日-20日, 宇宙航空研究開発機構宇宙科学研究本部)
The molecular dynamics (MD) simulation is performed to calculate complete angular distributions of sputtered carbon unde

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::bb6d633ca148135d7f99bb3abeb481c2
http://id.nii.ac.jp/1696/00016768/

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電離層プラズマ流を利用した姿勢制御のためのトルク測定およびホールスラスタにおけるスワールトルク計測

Autor: Koizumi, Hiroyuki, Kuninaka, Hitoshi, Nishida, Michio

Publikováno v: 宇宙輸送シンポジウム平成19年度 = Proceedings of Space Transportation Symposium FY2007. :443-446

平成19年度宇宙輸送シンポジウム（2008年1月28日-29日. 宇宙航空研究開発機構宇宙科学研究本部）, 相模原市, 神奈川県
Space Transportation Symposium FY2007 (January 28-29, 2008. Institute of Space and Astro

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::8c741aa0b23c1dc518423bc75951ba44
http://id.nii.ac.jp/1696/00016926/

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Toward sputtering analysis for ion engine accelerator grid

Autor: Hyakutake, Toru, Nishida, Michio, Kenmotsu, Takahiro, Muramoto, Tetsuya

Publikováno v: 宇宙航空研究開発機構特別資料: イオン加速グリッド耐久認定用数値解析JIEDI(JAXA Ion Engine Development Initiatives)ツールの研究開発ワークショップ 2006年度報告書 = JAXA Special Publication: Annual Report of Workshop on Research and Development of JIEDI (JAXA Ion Engine Development Initiatives) Tool for Numerical Evaluation of Ion Engine Grid Lifetime, FY2006. :59-63

本研究では、これらのプログラムコードをイオンエンジン加速グリッドのビーム解析に適用するとともに、その解析に必要な低エネルギーイオンにおけるスパッタリング率をシミュレー�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::65525f5ca88da908bdf1554464d59ea1
http://id.nii.ac.jp/1696/00005845/

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Modeling of the internal flow of an arcjet thruster and the review of numerical analyses

Autor: Nishida, Michio

Publikováno v: 宇宙輸送シンポジウム平成15年度 = Proceedings of Space Transportation Symposium FY2003. :368-371

資料番号: AA0047118091

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::ed30d5f8d3dd13935c2c9d6ad5c76224
http://id.nii.ac.jp/1696/00017315/

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Viscous Shock Layer Studies of a Super Orbital Reentry Capsule Using a Multi Vibrational Temperature Model

Autor: Doihara, Ryouji, Nishida, Michio

Publikováno v: The Institute of Space and Astronautical Science report. S.P. : Aerodynamics, Thermophysics, Thermal Protection, Flight System Analysis and Design of Asteroid Sample Return Capsule. 17:83-91

Numerical studies of the shock layer of a super orbital reentry capsule have been conducted by using thermochemical nonequilibrium VSL (Viscous Shock Layer) equations. In the present analysis, vibrational temperature has been treated as individual mo

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::f391f5afbedbaca74043ad88a95cc876
http://id.nii.ac.jp/1696/00033237/

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A Thermochemical Nonequilibrium Flow around a Super Orbital Reentry Capsule with Ablation

Autor: Doihara, Ryouji, Nishida, Michio

The aerodynamic heating to the super orbital reentry capsule of MUSES-C with ablation was numerically studied by using thermochemical nonequilibrium full viscous shock layer (VSL) equations. An 11 air-species model was used for non-ablating boundary

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::18140ce745b79a4d0211200449ddf796
http://id.nii.ac.jp/1696/00033234/

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