{"created":"2023-06-20T15:03:36.649852+00:00","id":32828,"links":{},"metadata":{"_buckets":{"deposit":"58f8734d-f785-4af3-bbf9-4573967add9b"},"_deposit":{"created_by":1,"id":"32828","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"32828"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00032828","sets":["1887:1890","1896:1898:1899:1912"]},"author_link":["411958","411961","411962","411963","411960","411959"],"item_9_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Theoretical Performance of Thrust Chamber"}]},"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1983-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"214","bibliographicPageStart":"193","bibliographicVolumeNumber":"6","bibliographic_titles":[{"bibliographic_title":"宇宙科学研究所報告. 特集: 液水/液酸エンジンの開発研究報告"}]}]},"item_9_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"エンジンの推力を示す各種パラメータをBrinkley, Glassmanの方法でプログラムした。このHPROPは火炎温度, 組成を比熱比を仮定せずに熱力学関数のみから算出しうるので有用である。反応速度が有限であることを考慮した非平衡計算はZucrowの方法で1次元で取扱いNOZFLAと命名した。不完全燃焼, いいかえれば燃焼室の中で部分的に反応が凍結している場合の熱伝導率への影響はSvehlaの方法でCONDYにまとめられている。この方法を用いてHST701,HST1001,TC-1002での再生冷却部の温度上昇と, 特性排気速度効率との相関を求め, 実験結果を説明するのに成功した。","subitem_description_type":"Abstract"}]},"item_9_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The computer program 'HPROP' has been completed to calculate the parameters of thrust performance of rocket engines on the basis of the Brinkley and G1assman methods. The program can afford to calculate the flame temperature, product composition etc. from the thermodynamical equilibrium relationships without any assumption of the specific heat ratio. The calculation of one-dimensional non-equilibrium expansion flow with chemical kinetics in rocket nozzle 'NOZFLA' also is programmed, based on the Zucrow's method. Further, the program 'CONDY' based on the Svehla's method can calculate the thermal conductivity of combustion gases in which the effect of incomplete combustion or partially frozen flow can be taken into account. The results calculated with this program explain successfully the experimental results of the tests HST-70l, HST-1001 and TC-1002 concerning the increase in the temperature of the coolant through the regenerative cooling passage and the efficiency of the characteristic exhaust velocity.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA0166597000","subitem_description_type":"Other"}]},"item_9_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙科学研究所"}]},"item_9_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Institute of Space and Astronautical Science"}]},"item_9_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0285-9920","subitem_source_identifier_type":"ISSN"}]},"item_9_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN00354485","subitem_source_identifier_type":"NCID"}]},"item_9_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"東京大学工学部"},{"subitem_text_value":"東海大学産業科学研究所"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"倉谷, 健治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小竹, 進"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"佐野, 妙子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"KURATANI, Kenji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"KOTAKE, Susumu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"SANO, Taeko","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":"2020-01-24"}],"displaytype":"detail","filename":"SA0166597.pdf","filesize":[{"value":"1.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA0166597.pdf","url":"https://jaxa.repo.nii.ac.jp/record/32828/files/SA0166597.pdf"},"version_id":"2d957143-ce4d-4bd2-925f-991ba74798cd"}]},"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":"departmental bulletin paper","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"理論性能計算","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"理論性能計算"}]},"item_type_id":"9","owner":"1","path":["1890","1912"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"32828","relation_version_is_last":true,"title":["理論性能計算"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T00:22:56.660990+00:00"}