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Microplasma thruster for ultra-small satellites: plasma chemical and aerodynamical aspects
http://hdl.handle.net/10131/9072
http://hdl.handle.net/10131/9072f0341407-3d32-46c4-8fc7-37f41c082eb4
名前 / ファイル | ライセンス | アクション |
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PureApplChem_80_2008_2013.pdf (756.2 kB)
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Item type | 学術雑誌論文 / Journal Article(1) | |||||
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公開日 | 2015-03-10 | |||||
タイトル | ||||||
タイトル | Microplasma thruster for ultra-small satellites: plasma chemical and aerodynamical aspects | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題 | plasma thrusters, electric propulsion, micropropulsion, microthrusters, microplasma, microdischarge, surface wave-excited plasma, micronozzle flow, microplasma jets, nano- and pico-satellites | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||
資源タイプ | journal article | |||||
著者 |
Takao, Yoshinori
× Takao, Yoshinori× Takahashi, Takeshi× Eriguchi, Koji× Ono, Kouichi |
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著者(ヨミ) | ||||||
識別子Scheme | WEKO | |||||
識別子 | 714 | |||||
識別子Scheme | e-Rad | |||||
識別子URI | https://kaken.nii.ac.jp/ja/search/?qm=80552661 | |||||
識別子 | 80552661 | |||||
姓名 | タカオ, ヨシノリ | |||||
著者(ヨミ) | ||||||
識別子Scheme | WEKO | |||||
識別子 | 19364 | |||||
姓名 | タカハシ, タケシ | |||||
著者(ヨミ) | ||||||
識別子Scheme | WEKO | |||||
識別子 | 19365 | |||||
姓名 | エリグチ, コウジ | |||||
著者(ヨミ) | ||||||
識別子Scheme | WEKO | |||||
識別子 | 19366 | |||||
姓名 | オノ, コウイチ | |||||
著者別名 | ||||||
識別子Scheme | WEKO | |||||
識別子 | 714 | |||||
識別子Scheme | e-Rad | |||||
識別子URI | https://kaken.nii.ac.jp/ja/search/?qm=80552661 | |||||
識別子 | 80552661 | |||||
姓名 | 鷹尾, 祥典 | |||||
著者別名 | ||||||
識別子Scheme | WEKO | |||||
識別子 | 19342 | |||||
姓名 | 高橋, 岳志 | |||||
著者別名 | ||||||
識別子Scheme | WEKO | |||||
識別子 | 19369 | |||||
姓名 | 江利口, 浩二 | |||||
著者別名 | ||||||
識別子Scheme | WEKO | |||||
識別子 | 19370 | |||||
姓名 | 斧, 髙一 | |||||
著者所属 | ||||||
Department of Aeronautics and Astronautics, Graduate School of Engineering, Kyoto University | ||||||
著者所属 | ||||||
Department of Aeronautics and Astronautics, Graduate School of Engineering, Kyoto University | ||||||
著者所属 | ||||||
Department of Aeronautics and Astronautics, Graduate School of Engineering, Kyoto University | ||||||
著者所属 | ||||||
Department of Aeronautics and Astronautics, Graduate School of Engineering, Kyoto University | ||||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | A microplasma thruster has been developed of electrothermal type using azimuthallysymmetric microwave-excited microplasmas. The microplasma source was ~2 mmin diameter and ~10 mm long, being operated at around atmospheric pressures; the micronozzlewas a converging-diverging type, having a throat ~0.2 mm in diameter and ~1 mmlong. Numerical and experimental results with Ar as a working gas demonstrated that thisminiature electrothermal thruster gives a thrust of >1 mN, a specific impulse of ~100 s, anda thrust efficiency of ~10% at a microwave power of <10 W, making it applicable to attitudecontroland station-keeping maneuver for a microspacecraft of <10 kg. | |||||
書誌情報 |
Pure and applied chemistry : the official journal of the International Union of Pure and Applied ChemistryChimie pure et appliqu?e 巻 80, 号 9, p. 2013-2023, 発行日 2008-09 |
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ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 00334545 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA00797859 | |||||
著者版フラグ | ||||||
出版タイプ | VoR | |||||
出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 |