{"created":"2023-06-20T14:36:58.046149+00:00","id":3337,"links":{},"metadata":{"_buckets":{"deposit":"89caae07-7c6c-4737-a5e7-ab35faf8ffc7"},"_deposit":{"created_by":1,"id":"3337","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"3337"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00003337","sets":["1398:1501:1503","1543:1827:1829","1887:1891","9:789:817:821"]},"author_link":["12939","12942","12940","12944","12945","12946","12943","12941"],"item_4_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"数値解析を用いた微小デブリ衝突の貫通限界曲線の取得状況"}]},"item_4_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2017-03-27","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"374","bibliographicPageStart":"367","bibliographicVolumeNumber":"JAXA-SP-16-011","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 第7回スペースデブリワークショップ講演資料集"},{"bibliographic_title":"JAXA Special Publication: Proceedings of the 7th Space Debris Workshop","bibliographic_titleLang":"en"}]}]},"item_4_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"第7回スペースデブリワークショップ (2016年10月18-20日. 宇宙航空研究開発機構調布航空宇宙センター(JAXA)(CAC)), 調布市, 東京","subitem_description_type":"Other"}]},"item_4_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"The 7th Space Debris Workshop (October 18-20, 2016. Chofu Aerospace Center, Japan Aerospace Exploration Agency (JAXA)(CAC)), Chofu, Tokyo, Japan","subitem_description_type":"Other"}]},"item_4_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"1991年、NASA/MSFCのKB.Hayashidaらは、1960年代にアポロ計画を中心にして検討されたメテオロイド防護技術としての2重板シールドシステム、いわゆる、Whippleバンパーシールドの貫通限界式、及びその後スペースデブリの脅威を踏まえて見直された式について概観した報告書を出している。そこで検討された式は、膨大な数の2段式軽ガス銃を中心とした試験結果に基づいたものであるが、1947年にF.L. Whippleが提案したアイデアを物理的に精査しメカニズムを明らかにすることによって、その防護システムの有効性を確認したものである。筆者らは、JAXA宇宙機設計標準推進委員会デブリ防護設計WGの活動の一環として、「スペースデブリ防護設計マニュアル」の作成を行っているが、その過程で、衛星設計に資するため、実験によるのではなく、数値解析によって貫通限界式の検討を行っている。また、バンパーの他に、電力ケーブルやハニカムパネルに対する検討も実施している。","subitem_description_type":"Abstract"}]},"item_4_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In 1991, K. B. Hayashida et al. at MSFC/NASA published a report reviewing the ballistic limit equations (BLE's) for the \"Double-Plate\", so-called Whipple bumper shield, which was investigated as a protection technology for the space vehicle from interplanetary meteoroid impacts mainly for the purpose of the Apollo program in 1960's. The report also reviews the modified equations applicable for the space debris impact, after the space debris problem emerged in 1970's. The BLE's referred to in the report were derived on the basis of vast amounts of hypervelocity impact tests using launchers like two-stage light gas gun, it was confirmed and proven that the Whipple bumper shield is indeed effective for the meteoroid protection by investigating and clarifying the mechanism of it, of which idea was proposed by F. L. Whipple in 1947. The authors have been writing the \"Design Manual on Space Debris Protection\" as an activity of the Working Group of the Space Debris Protection Design at JAXA, and they tried to derive the ballistic limit curves (equations) of small projectile impacts on the \"Double-Sheet\" targets, power cables and honeycomb panels only by the numerical analysis, not by the experiment.","subitem_description_type":"Other"}]},"item_4_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_type":"Other"}]},"item_4_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color illustrations","subitem_description_type":"Other"}]},"item_4_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA1630052029","subitem_description_type":"Other"}]},"item_4_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: JAXA-SP-16-011","subitem_description_type":"Other"}]},"item_4_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構(JAXA)"}]},"item_4_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_4_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-113X","subitem_source_identifier_type":"ISSN"}]},"item_4_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11984031","subitem_source_identifier_type":"NCID"}]},"item_4_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"伊藤忠テクノソリューションズ株式会社(CTC)"},{"subitem_text_value":"伊藤忠テクノソリューションズ株式会社(CTC)"},{"subitem_text_value":"宇宙航空研究開発機構(JAXA)"},{"subitem_text_value":"宇宙航空研究開発機構(JAXA)"}]},"item_4_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"ITOCHU Techno-Solutions Corporation (CTC)"},{"subitem_text_language":"en","subitem_text_value":"ITOCHU Techno-Solutions Corporation (CTC)"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"竹場, 敦史"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"片山, 雅英"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"仁田, 工美"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"東出, 真澄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takeba, Atsushi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Katayama, Masahide","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nitta, Kumi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Higashide, Masumi","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-15"}],"displaytype":"detail","filename":"AA1630052029.pdf","filesize":[{"value":"2.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"AA1630052029.pdf","url":"https://jaxa.repo.nii.ac.jp/record/3337/files/AA1630052029.pdf"},"version_id":"979c5b69-d4cb-4016-b3c0-ca6ca001df4e"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"conference object","resourceuri":"http://purl.org/coar/resource_type/c_c94f"}]},"item_title":"Current status of the estimation of the ballistic limit curves by performing numerical analyses of the small-size space debris impacts","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Current status of the estimation of the ballistic limit curves by performing numerical analyses of the small-size space debris impacts","subitem_title_language":"en"}]},"item_type_id":"4","owner":"1","path":["821","1503","1829","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2017-05-08"},"publish_date":"2017-05-08","publish_status":"0","recid":"3337","relation_version_is_last":true,"title":["Current status of the estimation of the ballistic limit curves by performing numerical analyses of the small-size space debris impacts"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:04:42.734068+00:00"}