{"_buckets": {"deposit": "947fa217-c72c-4880-bfbf-1b75b1f29a09"}, "_deposit": {"created_by": 1, "id": "1904", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "1904"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00001904", "sets": ["58", "1425", "1893"]}, "author_link": ["1317", "1314", "1313", "1316", "1315", "1318"], "item_3_alternative_title_2": {"attribute_name": "その他のタイトル（英）", "attribute_value_mlt": [{"subitem_alternative_title": "Burning rate control of AP composite propellants: Effects of TiO2 additive"}]}, "item_3_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2016-03-02", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "59", "bibliographicPageStart": "55", "bibliographicVolumeNumber": "JAXA-RR-15-004", "bibliographic_titles": [{"bibliographic_title": "宇宙航空研究開発機構研究開発報告: 高エネルギー物質研究会: 平成27年度研究成果報告書"}, {"bibliographic_title": "JAXA Research and Development Report", "bibliographic_titleLang": "en"}]}]}, "item_3_description_16": {"attribute_name": "抄録", "attribute_value_mlt": [{"subitem_description": "本研究の目的は，固体ロケットにおける人工衛星輸送能力を左右する第3段固体ロケットモータ用固体推進薬の高性能化である。第3段用固体推進薬の高性能化には，Al粒子の集塊抑制及び低燃焼速度化が要求される。本研究では，Al粒子と異なる集塊特性を持つMg-Al粒子を用いてAl粒子の集塊抑制を検討している。しかしながら，Mg-Al系推進薬はAl系推進薬と比較して燃焼速度が高い。低燃焼速度かつAl粒子の燃焼促進を図るために，燃焼負触媒を加える手法が挙げられる。本報告では，Al系推進薬及びMg-Al系推進薬にTiO2粒子を添加し，固体推進薬の燃焼速度に対するTiO2粒子添加の効果を取得した。", "subitem_description_type": "Abstract"}]}, "item_3_description_17": {"attribute_name": "抄録（英）", "attribute_value_mlt": [{"subitem_description": "To improve the propulsion performance of third stage solid rocket motor, high-performance solid propellant is required. This propellant is needed to inhibit Al agglomeration on the combustion surface and decrease burning rate. In this study, Mg-Al particles are incorporated into the general solid propellants in order to reduce Al agglomeration since the agglomeration characteristics of Mg-Al are different to Al. However, the burning rate of propellants containing Mg-Al particles is higher than that containing Al. To control the burning rate solid propellants, the catalysts are generally added. In this study, the effects of titanium oxide as a catalyst to burning rate of AP composite propellants are obtained.", "subitem_description_type": "Other"}]}, "item_3_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_3_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_3_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA1530055008", "subitem_description_type": "Other"}]}, "item_3_description_33": {"attribute_name": "レポート番号", "attribute_value_mlt": [{"subitem_description": "レポート番号: JAXA-RR-15-004", "subitem_description_type": "Other"}]}, "item_3_publisher_8": {"attribute_name": "出版者", "attribute_value_mlt": [{"subitem_publisher": "宇宙航空研究開発機構(JAXA)"}]}, "item_3_publisher_9": {"attribute_name": "出版者（英）", "attribute_value_mlt": [{"subitem_publisher": "Japan Aerospace Exploration Agency (JAXA)"}]}, "item_3_source_id_21": {"attribute_name": "ISSN", "attribute_value_mlt": [{"subitem_source_identifier": "1349-1113", "subitem_source_identifier_type": "ISSN"}]}, "item_3_source_id_24": {"attribute_name": "書誌レコードID", "attribute_value_mlt": [{"subitem_source_identifier": "AA1192675X", "subitem_source_identifier_type": "NCID"}]}, "item_3_text_34": {"attribute_name": "メタデータ提供者", "attribute_value_mlt": [{"subitem_text_value": "メタデータ提供者: JAXA"}]}, "item_3_text_35": {"attribute_name": "JAXAカテゴリ", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ: 研究開発報告"}]}, "item_3_text_36": {"attribute_name": "JAXAカテゴリ2", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ2: IS"}]}, "item_3_text_38": {"attribute_name": "ＮＡＳＡ分類コード", "attribute_value_mlt": [{"subitem_text_value": "NASA分類コード: 28"}]}, "item_3_text_39": {"attribute_name": "ＮＡＳＡ分類表目標", "attribute_value_mlt": [{"subitem_text_value": "NASA分類: Propellants and Fuels"}]}, "item_3_text_40": {"attribute_name": "jaxa出版物種類", "attribute_value_mlt": [{"subitem_text_value": "jaxa出版物種類: RR"}]}, "item_3_text_41": {"attribute_name": "jaxa出版物シリーズ", "attribute_value_mlt": [{"subitem_text_value": "jaxa出版物シリーズ: 003"}]}, "item_3_text_43": {"attribute_name": "DSpaceコレクション番号", "attribute_value_mlt": [{"subitem_text_value": "DSpaceコレクション番号: 10"}]}, "item_3_text_6": {"attribute_name": "著者所属", "attribute_value_mlt": [{"subitem_text_value": "宇宙航空研究開発機構宇宙科学研究所宇宙飛翔工学研究系(JAXA)(ISAS)"}, {"subitem_text_value": "総合研究大学院大学(SOKENDAI)"}, {"subitem_text_value": "宇宙航空研究開発機構宇宙科学研究所宇宙飛翔工学研究系(JAXA)(ISAS)"}]}, "item_3_text_7": {"attribute_name": "著者所属（英）", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "Department of Space Flight Systems, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"}, {"subitem_text_language": "en", "subitem_text_value": "The Graduate University for Advanced Studies (SOKENDAI)"}, {"subitem_text_language": "en", "subitem_text_value": "Department of Space Flight Systems, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)"}]}, "item_creator": {"attribute_name": "著者", "attribute_type": "creator", "attribute_value_mlt": [{"creatorNames": [{"creatorName": "松本, 幸太郎"}], "nameIdentifiers": [{"nameIdentifier": "1313", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "岩崎, 祥大"}], "nameIdentifiers": [{"nameIdentifier": "1314", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "羽生, 宏人"}], "nameIdentifiers": [{"nameIdentifier": "1315", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Matsumoto, Kotaro", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "1316", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Iwasaki, Akihiro", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "1317", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Habu, Hiroto", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "1318", "nameIdentifierScheme": "WEKO"}]}]}, "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", "download_preview_message": "", "file_order": 0, "filename": "AA1530055008.pdf", "filesize": [{"value": "754.9 kB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_free", "mimetype": "application/pdf", "size": 754900.0, "url": {"label": "AA1530055008.pdf", "url": "https://jaxa.repo.nii.ac.jp/record/1904/files/AA1530055008.pdf"}, "version_id": "9006458b-8781-4784-85a7-e1b70bc0dcef"}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "Aluminum", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Magnalium", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Solid Propellant", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Burning Rate", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Titanium Oxide", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}]}, "item_language": {"attribute_name": "言語", "attribute_value_mlt": [{"subitem_language": "jpn"}]}, "item_resource_type": {"attribute_name": "資源タイプ", "attribute_value_mlt": [{"resourcetype": "technical report", "resourceuri": "http://purl.org/coar/resource_type/c_18gh"}]}, "item_title": "AP系コンポジット推進薬の燃焼速度制御: TiO2添加の効果", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "AP系コンポジット推進薬の燃焼速度制御: TiO2添加の効果"}]}, "item_type_id": "3", "owner": "1", "path": ["58", "1425", "1893"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/1904", "pubdate": {"attribute_name": "公開日", "attribute_value": "2016-03-18"}, "publish_date": "2016-03-18", "publish_status": "0", "recid": "1904", "relation": {}, "relation_version_is_last": true, "title": ["AP系コンポジット推進薬の燃焼速度制御: TiO2添加の効果"], "weko_shared_id": -1}