{"_buckets": {"deposit": "634ded4d-39e8-4a45-a336-22869c0f4a30"}, "_deposit": {"id": "30071", "owners": [], "pid": {"revision_id": 0, "type": "depid", "value": "30071"}, "status": "published"}, "_oai": {"id": "oai:nagoya.repo.nii.ac.jp:00030071"}, "item_10_biblio_info_6": {"attribute_name": "\u66f8\u8a8c\u60c5\u5831", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2020-01", "bibliographicIssueDateType": "Issued"}, "bibliographicIssueNumber": "1", "bibliographicPageEnd": "77", "bibliographicPageStart": "68", "bibliographicVolumeNumber": "36", "bibliographic_titles": [{"bibliographic_title": "Journal of Propulsion and Power"}]}]}, "item_10_description_4": {"attribute_name": "\u6284\u9332", "attribute_value_mlt": [{"subitem_description": "The effects of hollow cathode position on thrust performances of a diverging-magnetic-field electrostatic thruster, which had a diverging magnetic field between a ring anode and a hollow cathode, were investigated. The hollow cathode was located in either a central or an external configuration. Based on the discharge current and direct thrust measurements, electrostatic and magnetic hybrid plasma acceleration was observed in the central cathode operation and even in the external cathode operation especially when magnetic field strength was less than 315 mT. However, the operating points were different: low discharge voltage\u00d7large discharge current in the central cathode operation, and high discharge voltage\u00d7small discharge current in the external cathode operation. This difference comes from electron-Hall parameter; the estimated electron-Hall parameter was about 50 in the central cathode operation, which was much lower than that of 3000 in the external cathode operation. By combining electromagnetic acceleration, the generated thrust can increase even with lower electron-Hall parameter operation. As a result, similar thrust performances were achieved in both cathode positions. Because of the hybrid plasma acceleration method, thrust density reached 50\u2009\u2009N/m^2, which is comparable or even higher than that of the conventional electrostatic thrusters.", "subitem_description_type": "Abstract"}]}, "item_10_description_5": {"attribute_name": "\u5185\u5bb9\u8a18\u8ff0", "attribute_value_mlt": [{"subitem_description": "Published Online:14 Nov 2019", "subitem_description_type": "Other"}]}, "item_10_publisher_32": {"attribute_name": "\u51fa\u7248\u8005", "attribute_value_mlt": [{"subitem_publisher": "American Institute of Aeronautics and Astronautics"}]}, "item_10_relation_11": {"attribute_name": "DOI", "attribute_value_mlt": [{"subitem_relation_type_id": {"subitem_relation_type_id_text": "https://doi.org/10.2514/1.B37636", "subitem_relation_type_select": "DOI"}}]}, "item_10_rights_12": {"attribute_name": "\u6a29\u5229", "attribute_value_mlt": [{"subitem_rights": "Copyright \u00a9 2019 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 eISSN 1533-3876 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_61": {"attribute_name": "ISSN\uff08print\uff09", "attribute_value_mlt": [{"subitem_source_identifier": "1533-3876", "subitem_source_identifier_type": "ISSN"}]}, "item_creator": {"attribute_name": "\u8457\u8005", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "Ichihara, Daisuke"}], "nameIdentifiers": [{"nameIdentifier": "99185", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Nakagawa, Yoshiya"}], "nameIdentifiers": [{"nameIdentifier": "99186", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Iwakawa, Akira"}], "nameIdentifiers": [{"nameIdentifier": "99187", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Sasoh, Akihiro"}], "nameIdentifiers": [{"nameIdentifier": "99188", "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": "2020-05-26"}], "displaytype": "detail", "download_preview_message": "", "file_order": 0, "filename": "JPP-B37636_AUTHOR_1_Revised.pdf", "filesize": [{"value": "1.3 MB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 1300000.0, "url": {"label": "JPP-B37636_AUTHOR_1_Revised", "url": "https://nagoya.repo.nii.ac.jp/record/30071/files/JPP-B37636_AUTHOR_1_Revised.pdf"}, "version_id": "3084fd82-56ca-46d0-8936-9443b29c8fa8"}]}, "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": "Central and External Cathode Operations in a Diverging-Magnetic-Field Electrostatic Thruster", "item_titles": {"attribute_name": "\u30bf\u30a4\u30c8\u30eb", "attribute_value_mlt": [{"subitem_title": "Central and External Cathode Operations in a Diverging-Magnetic-Field Electrostatic Thruster"}]}, "item_type_id": "10", "owner": "1", "path": ["320/321/322"], "permalink_uri": "http://hdl.handle.net/2237/00032257", "pubdate": {"attribute_name": "\u516c\u958b\u65e5", "attribute_value": "2020-05-26"}, "publish_date": "2020-05-26", "publish_status": "0", "recid": "30071", "relation": {}, "relation_version_is_last": true, "title": ["Central and External Cathode Operations in a Diverging-Magnetic-Field Electrostatic Thruster"], "weko_shared_id": null}