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  1. B200 工学部/工学研究科
  2. B200a 雑誌掲載論文
  3. 学術雑誌

Ten-Ampere-Level, Applied-Field-Dominant Operation in Magnetoplasmadynamic Thrusters

http://hdl.handle.net/2237/26589
http://hdl.handle.net/2237/26589
6ab512b9-bd56-4656-83fa-b2c747790a2f
名前 / ファイル ライセンス アクション
JPP-B36179_AUTHOR_1_Author_modified.pdf JPP-B36179_AUTHOR_1_Author_modified.pdf (679.1 kB)
Item type 学術雑誌論文 / Journal Article(1)
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

WEKO 72214

en Ichihara, Daisuke

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Uno, Tomoki

× Uno, Tomoki

WEKO 72215

en Uno, Tomoki

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Kataoka, Hisashi

× Kataoka, Hisashi

WEKO 72216

en Kataoka, Hisashi

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Jeong, Jaehun

× Jeong, Jaehun

WEKO 72217

en Jeong, Jaehun

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Iwakawa, Akira

× Iwakawa, Akira

WEKO 72218

en Iwakawa, Akira

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Sasoh, Akihiro

× Sasoh, Akihiro

WEKO 72219

en Sasoh, Akihiro

Search repository
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
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
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