WEKO3
アイテム
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オーバラップクラスタノズル燃焼試験
https://jaxa.repo.nii.ac.jp/records/38678
https://jaxa.repo.nii.ac.jp/records/38678f043c47e-13a4-4b34-8c87-88b9b00b83d4
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-09-28 | |||||
タイトル | ||||||
タイトル | オーバラップクラスタノズル燃焼試験 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Overlap Cluster Nozzle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Firing Test | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Hot Fire Test of Overlap Cluster Nozzle | |||||
著者 |
増田, 井出夫
× 増田, 井出夫× 藤井, 剛× 畑井, 啓吾× 香河, 英史× 池田, 博英× 草間, 光治× Masuda, Ideo× Fujii, Go× Hatai, Keigo× Kagawa, Hideshi× Ikeda, Hirohide× Kusama, Mitsuharu |
|||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
AES | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
AES | ||||||
出版者 | ||||||
出版者 | 日本航空宇宙学会(JSASS) | |||||
出版者(英) | ||||||
出版者 | The Japan Society for Aeronautical and Space Sciences (JSASS) | |||||
書誌情報 |
第58回宇宙科学技術連合講演会講演集 en : Proceedings of 58th Space Sciences and Technology Conference 発行日 2014-11 |
|||||
会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 第58回宇宙科学技術連合講演会(2014年11月12日-14日. 長崎ブリックホール), 長崎市, 長崎県 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | "We choose a new type of cluster nozzle for satellites, from the perspective of improved performance within the restricted installation area of rockets. The new nozzles are considered much more efficient for the larger nozzle expansion area ratio than existing ones. Given the concerns over degraded performance due to a slower flow of exhaust gas caused by shock waves in the overlapped area between the modules that constitute a cluster nozzle, we evaluated the effect of each module’s overlap ratio on nozzle performance based on an examination using nitrogen gas. Our experimental and analytical results by cold gas revealed that the plug cluster nozzle having a low overlap ratio offers better performance than the bell nozzle having the same effective expansion ratio. In order to understand the combustion gas characteristics of the plug cluster nozzle, we plan to perform firing tests. We describe the firing test nozzle, test equipment and the firing test of the ignitor and the injector for the nozzle in this paper." | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AC1500037000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JSASS-2014-4203 |