{"_buckets": {"deposit": "193e6e35-aec9-4202-aa92-c8def45135d2"}, "_deposit": {"id": "24380", "owners": [], "pid": {"revision_id": 0, "type": "depid", "value": "24380"}, "status": "published"}, "_oai": {"id": "oai:nagoya.repo.nii.ac.jp:00024380"}, "item_10_biblio_info_6": {"attribute_name": "\u66f8\u8a8c\u60c5\u5831", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2017-03", "bibliographicIssueDateType": "Issued"}, "bibliographicIssueNumber": "2", "bibliographicPageEnd": "369", "bibliographicPageStart": "360", "bibliographicVolumeNumber": "33", "bibliographic_titles": [{"bibliographic_title": "Journal of Propulsion and Power"}]}]}, "item_10_description_4": {"attribute_name": "\u6284\u9332", "attribute_value_mlt": [{"subitem_description": "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\u2215s 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 \u201cswirl acceleration\u201d model. Such operation could be useful for near-future high-power electric propulsion applications.", "subitem_description_type": "Abstract"}]}, "item_10_identifier_60": {"attribute_name": "URI", "attribute_value_mlt": [{"subitem_identifier_type": "DOI", "subitem_identifier_uri": "https://doi.org/10.2514/1.B36179"}, {"subitem_identifier_type": "HDL", "subitem_identifier_uri": "http://hdl.handle.net/2237/26589"}]}, "item_10_publisher_32": {"attribute_name": "\u51fa\u7248\u8005", "attribute_value_mlt": [{"subitem_publisher": "American Institute of Aeronautics and Astronautics"}]}, "item_10_rights_12": {"attribute_name": "\u6a29\u5229", "attribute_value_mlt": [{"subitem_rights": "Copyright \u00a9 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."}]}, "item_10_select_15": {"attribute_name": "\u8457\u8005\u7248\u30d5\u30e9\u30b0", "attribute_value_mlt": [{"subitem_select_item": "author"}]}, "item_10_source_id_7": {"attribute_name": "ISSN", "attribute_value_mlt": [{"subitem_source_identifier": "0748-4658", "subitem_source_identifier_type": "ISSN"}]}, "item_creator": {"attribute_name": "\u8457\u8005", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "Ichihara, Daisuke"}], "nameIdentifiers": [{"nameIdentifier": "72214", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Uno, Tomoki"}], "nameIdentifiers": [{"nameIdentifier": "72215", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Kataoka, Hisashi"}], "nameIdentifiers": [{"nameIdentifier": "72216", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Jeong, Jaehun"}], "nameIdentifiers": [{"nameIdentifier": "72217", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Iwakawa, Akira"}], "nameIdentifiers": [{"nameIdentifier": "72218", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Sasoh, Akihiro"}], "nameIdentifiers": [{"nameIdentifier": "72219", "nameIdentifierScheme": "WEKO"}]}]}, "item_files": {"attribute_name": "\u30d5\u30a1\u30a4\u30eb\u60c5\u5831", "attribute_type": "file", "attribute_value_mlt": [{"accessrole": "open_date", "date": [{"dateType": "Available", "dateValue": "2018-02-22"}], "displaytype": "detail", "download_preview_message": "", "file_order": 0, "filename": "JPP-B36179_AUTHOR_1_Author_modified.pdf", "filesize": [{"value": "679.1 kB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 679100.0, "url": {"label": "JPP-B36179_AUTHOR_1_Author_modified.pdf", "url": "https://nagoya.repo.nii.ac.jp/record/24380/files/JPP-B36179_AUTHOR_1_Author_modified.pdf"}, "version_id": "4f7faf8a-003a-40cb-97f3-51a82320d790"}]}, "item_language": {"attribute_name": "\u8a00\u8a9e", "attribute_value_mlt": [{"subitem_language": "eng"}]}, "item_resource_type": {"attribute_name": "\u8cc7\u6e90\u30bf\u30a4\u30d7", "attribute_value_mlt": [{"resourcetype": "journal article", "resourceuri": "http://purl.org/coar/resource_type/c_6501"}]}, "item_title": "Ten-Ampere-Level, Applied-Field-Dominant Operation in Magnetoplasmadynamic Thrusters", "item_titles": {"attribute_name": "\u30bf\u30a4\u30c8\u30eb", "attribute_value_mlt": [{"subitem_title": "Ten-Ampere-Level, Applied-Field-Dominant Operation in Magnetoplasmadynamic Thrusters"}]}, "item_type_id": "10", "owner": "1", "path": ["320/321/322"], "permalink_uri": "http://hdl.handle.net/2237/26589", "pubdate": {"attribute_name": "\u516c\u958b\u65e5", "attribute_name_i18n": "\u516c\u958b\u65e5", "attribute_value": "2017-06-07"}, "publish_date": "2017-06-07", "publish_status": "0", "recid": "24380", "relation": {}, "relation_version_is_last": true, "title": ["Ten-Ampere-Level, Applied-Field-Dominant Operation in Magnetoplasmadynamic Thrusters"], "weko_shared_id": null}