{"created":"2023-06-20T15:10:22.015995+00:00","id":39949,"links":{},"metadata":{"_buckets":{"deposit":"5b28df84-5805-4a3e-a7bc-26507fc72d8b"},"_deposit":{"created_by":1,"id":"39949","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"39949"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00039949","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["445704","445714","445709","445711","445712","445713","445716","445715","445706","445710","445708","445705","445707","445717"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Gas jet pressure controller for NAL supersonic wind tunnel test and thrust test stand for supersonic jet nozzles"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1997-05","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"15","bibliographicPageStart":"1","bibliographicVolumeNumber":"710","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所資料"},{"bibliographic_title":"Technical Memorandum of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"無人宇宙往還機HOPE(H-2 Orbiting Plane)が地球大気に再突入する場合にガスジェットによる姿勢制御を行う。この時ガスジェットの推力やそれによるモーメント以外に、他方向の力やモーメントにも影響を与える。これらの空力干渉を1m×1m超音速風洞試験で調べるために、ガスジェット供給装置と超音速ノズル推力測定装置を製作した。またそれらの性能を試験した。ガスジェット供給装置は約5MPaまで安定した圧力で窒素ガスを供給できた。この装置では、1から5voltの制御電圧を印加することにより圧力制御ができる。また超音速ノズル推力測定装置を用いて、マッハ数M(sub j)=2.5、3.0、3.5および4.0の各超音速ノズル模型の推力を測定した結果、測定値と理論値は良く一致した。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A gas supply device was constructed to supply the reaction control nozzle of the Japanese space shuttle model, HOPE (H-2 Orbiting Plane), with nitrogen gas at an arbitrary pressure. The variation of the supplied gas pressure is controlled up to 5 MPa manually or electrically by imposing a control voltage. The variation of the instantaneous temperature, the pressure and the flow rate of the supplied gas are recorded to evaluate the control performance of the device. The supplied gas pressure is controlled to a constant value within one second, while the temperature varied greatly over five seconds. To measure the thrust of the reaction gas jet a test stand without interaction by the supplied high pressure gas through the piping was devised. The thrust of supersonic jet nozzles for jet Mach number 2.5, 3.0, 3.5 and 4.0 showed almost the same values as theoretically predicted.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001065000","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: NAL TM-710","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0452-2982","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":"AN00314334","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所 空気力学部"},{"subitem_text_value":"航空宇宙技術研究所 空気力学部"},{"subitem_text_value":"航空宇宙技術研究所 空気力学部"},{"subitem_text_value":"航空宇宙技術研究所 空気力学部"},{"subitem_text_value":"航空宇宙技術研究所 空気力学部"},{"subitem_text_value":"航空宇宙技術研究所 空気力学部"},{"subitem_text_value":"航空宇宙技術研究所 空気力学部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aerodynamics Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"渡辺, 光則"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"浜本, 滋"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"原, 亘利"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"楯, 篤志"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野田, 順一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"平林, 則明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"吉永, 崇"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Watanabe, Mitsunori","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hamamoto, Shigeru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hara, Nobutoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tate, Atsushi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Noda, Junichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hirabayashi, Noriaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yoshinaga, Takashi","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":"2020-01-27"}],"displaytype":"detail","filename":"naltm0000710.pdf","filesize":[{"value":"4.7 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm0000710.pdf","url":"https://jaxa.repo.nii.ac.jp/record/39949/files/naltm0000710.pdf"},"version_id":"77f1b741-9631-4fdf-a487-b1d7d62293b7"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"超音速風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"ガスジェット供給装置","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速ノズル","subitem_subject_scheme":"Other"},{"subitem_subject":"推力測定装置","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE","subitem_subject_scheme":"Other"},{"subitem_subject":"H-2ロケット打上げ型有翼回収機","subitem_subject_scheme":"Other"},{"subitem_subject":"ガスジェット姿勢制御システム","subitem_subject_scheme":"Other"},{"subitem_subject":"ガスジェット圧力制御装置","subitem_subject_scheme":"Other"},{"subitem_subject":"空力干渉","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"gas jet supply device","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic jet nozzles","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thrust test stand","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"H 2 orbiting plane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reaction control system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"gas jet pressure controller","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic interference","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":"NAL超音速風洞用ガスジェット供給装置および超音速ノズル推力測定装置","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"NAL超音速風洞用ガスジェット供給装置および超音速ノズル推力測定装置"}]},"item_type_id":"3","owner":"1","path":["1893","1916"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"39949","relation_version_is_last":true,"title":["NAL超音速風洞用ガスジェット供給装置および超音速ノズル推力測定装置"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:18:09.299297+00:00"}