{"created":"2023-06-20T15:07:28.942467+00:00","id":36852,"links":{},"metadata":{"_buckets":{"deposit":"206dbefc-b1a3-4219-bd63-28586bcb894a"},"_deposit":{"created_by":1,"id":"36852","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"36852"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00036852","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["477875","477873","477876","477874"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"HYFLEX onboard measurement program"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1996-09","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"128","bibliographicPageStart":"118","bibliographicVolumeNumber":"32","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_5_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":"24-25 Jul. 1996","subitem_description_type":"Other"}]},"item_5_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":"24-25 Jul. 1996","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"極超音速飛行実験においては、5分間程度の持続的な極超音速飛行時間が確保されるため、往還機に重要なM＞10領域の空力、空力加熱特性データが質量とも充実したレベルで得られることが期待された。機上計測項目の選定においては、これら極超音速領域の実在気体効果を含む空力、空力加熱特性データ、熱構造の特性評価用データ、および主目的のひとつである揚力飛行体の基本技術評価に関わるデータ(姿勢・軌道制御に関するデータなど)などを抽出し、バス系の計測項目をあわせて約250チャンネルの計測計画をたてた。各計測項目を選定した基準、設計のための事前解析・試験、各項目の計測系仕様について述べる。具体的議論は主に実験計測系に限った。また、計測の目的は宇宙往還機設計などへ利用できる予測ツール・手法の確立に資することである。そのため、地上での試験やCFD(数値流体力学)による予測とフライトデータとを比較するが、その際に飛行時の大気状態を可能な限り正確に把握する必要がある。今回は大気状態量の特定のため、NOAA衛星のリモートセンシングデータを使用し推定精度を上げることを試みた。これを含むデータ解析計画の概略を述べた。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In the HYFLEX (Hypersonic Flight Experiment), a consecutive hypersonic flight duration of some five minutes is secured. Therefore, it is expected to get the hypersonic aerodynamic/aerothermodynamic performance data good enough in both qualitative and quantitative sense for the region in which M is greater than ten, where best performance is crucial for the reusable space vehicles. Selection of the measurement items for the onboard measurement system was made among both aerodynamics and aerothermodynamics including the real gas effects, thermo-structural evaluation data, basic data for evaluation of lifting body technology (guidance, navigation and control) etc. consisting of some 250 channels in total. Decision to select measurement items, the analyses and tests for design and confirmation, specifications of each items are outlined and discussed in this paper. But mostly measurement mission items are discussed in this paper. Major objective of HYFLEX onboard measurement is to contribute to establishing reliable prediction/design methods for the winged space vehicles. To do this, the comparison between the flight data and the predictions made in advance based on ground test and analyses is indispensable. For the meaningful comparison, the atmospheric condition along flight path must be known accurately enough. In HYFLEX, the utilization of the remotely sensed atmospheric data by NOAA meteorological satellite was planned to raise the inference accuracy. Data analysis program is briefly presented.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000584014","subitem_description_type":"Other"}]},"item_5_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL SP-32","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","subitem_source_identifier_type":"ISSN"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN10097345","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"井上, 安敏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"白水, 正男"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Inoue, Yasutoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shirouzu, Masao","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":"2020-02-10"}],"displaytype":"detail","filename":"nalsp0032014.pdf","filesize":[{"value":"886.8 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0032014.pdf","url":"https://jaxa.repo.nii.ac.jp/record/36852/files/nalsp0032014.pdf"},"version_id":"e244e5bd-406d-4c22-87f9-00ddbcb673ee"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"極超音速飛行実験","subitem_subject_scheme":"Other"},{"subitem_subject":"HYFLEX","subitem_subject_scheme":"Other"},{"subitem_subject":"実在気体効果","subitem_subject_scheme":"Other"},{"subitem_subject":"空力特性","subitem_subject_scheme":"Other"},{"subitem_subject":"空力加熱特性","subitem_subject_scheme":"Other"},{"subitem_subject":"再突入機","subitem_subject_scheme":"Other"},{"subitem_subject":"熱防護系","subitem_subject_scheme":"Other"},{"subitem_subject":"温度計測","subitem_subject_scheme":"Other"},{"subitem_subject":"圧力計測","subitem_subject_scheme":"Other"},{"subitem_subject":"歪計測","subitem_subject_scheme":"Other"},{"subitem_subject":"反射計","subitem_subject_scheme":"Other"},{"subitem_subject":"リモートセンシング","subitem_subject_scheme":"Other"},{"subitem_subject":"オンボード計測システム","subitem_subject_scheme":"Other"},{"subitem_subject":"数値流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"NOAA","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic flight experiment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"HYFLEX","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"real gas effect","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerothermodynamic characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reentry vehicle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thermal protection","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thermometry","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pressure measurement","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"strain measurement","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reflectometer","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"remote sensing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"onboard measurement system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"NOAA","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":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"HYFLEXの計測計画","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"HYFLEXの計測計画"}]},"item_type_id":"5","owner":"1","path":["1891","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"36852","relation_version_is_last":true,"title":["HYFLEXの計測計画"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:30:38.679527+00:00"}