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Ten-Ampere-Level, Applied-Field-Dominant Operation in Magnetoplasmadynamic Thrusters
http://hdl.handle.net/2237/26589
http://hdl.handle.net/2237/265896ab512b9-bd56-4656-83fa-b2c747790a2f
名前 / ファイル | ライセンス | アクション |
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JPP-B36179_AUTHOR_1_Author_modified.pdf (679.1 kB)
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Item type | 学術雑誌論文 / Journal Article(1) | |||||
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公開日 | 2017-06-07 | |||||
タイトル | ||||||
タイトル | Ten-Ampere-Level, Applied-Field-Dominant Operation in Magnetoplasmadynamic Thrusters | |||||
言語 | en | |||||
著者 |
Ichihara, Daisuke
× Ichihara, Daisuke× Uno, Tomoki× Kataoka, Hisashi× Jeong, Jaehun× Iwakawa, Akira× Sasoh, Akihiro |
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アクセス権 | ||||||
アクセス権 | open access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_abf2 | |||||
権利 | ||||||
言語 | en | |||||
権利情報 | Copyright © 2016 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the ISSN 0748-4658 (print) or 1533-3876 (online) to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. | |||||
抄録 | ||||||
内容記述 | In this paper, applied-field magnetoplasmadynamic thrusters were operated with a discharge current lower than 20 A and an argon propellant flow rate under 4.0 mg∕s by using a thermionic electron emission-type hollow cathode. Both axisymmetric and rectangular channel configurations were examined. The characteristic value of the ratio of the applied-field electromagnetic thrust to the self-field electromagnetic thrust, which was a maximum of approximately 50 in previous research, increased to more than 800 in this study, whereas the specific power was in approximately the same range as in previous studies. The trends of thrust and discharge voltage were explained by referring to the “swirl acceleration” model. Such operation could be useful for near-future high-power electric propulsion applications. | |||||
言語 | en | |||||
内容記述タイプ | Abstract | |||||
出版者 | ||||||
言語 | en | |||||
出版者 | American Institute of Aeronautics and Astronautics | |||||
言語 | ||||||
言語 | eng | |||||
資源タイプ | ||||||
資源タイプresource | http://purl.org/coar/resource_type/c_6501 | |||||
タイプ | journal article | |||||
出版タイプ | ||||||
出版タイプ | AM | |||||
出版タイプResource | http://purl.org/coar/version/c_ab4af688f83e57aa | |||||
DOI | ||||||
関連タイプ | isVersionOf | |||||
識別子タイプ | DOI | |||||
関連識別子 | https://doi.org/10.2514/1.B36179 | |||||
ISSN | ||||||
収録物識別子タイプ | PISSN | |||||
収録物識別子 | 0748-4658 | |||||
書誌情報 |
en : Journal of Propulsion and Power 巻 33, 号 2, p. 360-369, 発行日 2017-03 |
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著者版フラグ | ||||||
値 | author | |||||
URI | ||||||
識別子 | https://doi.org/10.2514/1.B36179 | |||||
識別子タイプ | DOI | |||||
URI | ||||||
識別子 | http://hdl.handle.net/2237/26589 | |||||
識別子タイプ | HDL |