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高圧燃焼下におけるLOX/LNG(メタン)同軸型噴射器の燃焼特性について
https://jaxa.repo.nii.ac.jp/records/38831
https://jaxa.repo.nii.ac.jp/records/38831b99e6823-9656-4fed-943f-0c9fcea8e326
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2016-09-21 | |||||
タイトル | ||||||
タイトル | 高圧燃焼下におけるLOX/LNG(メタン)同軸型噴射器の燃焼特性について | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | LNG | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | methane | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | shear coaxial element | |||||
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 | Study on combustion characteristics of LOX/methane co-axial type injector under high pressure condition | |||||
著者 |
淺川, 弘也
× 淺川, 弘也× 南里, 秀明× 増田, 井出夫× 篠原, 流× 石原, 康弘× 坂口, 裕之× Asakawa, Hiroya× Nanri, Hideaki× Masuda, Ideo× Shinohara, Ryu× Ishikawa, Yasuhiro× Sakaguchi, Hiroyuki |
|||||
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 | ||||||
株式会社IHI | ||||||
著者所属 | ||||||
株式会社IHI | ||||||
著者所属 | ||||||
株式会社IHI | ||||||
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 | ||||||
IHI Corporation | ||||||
著者所属(英) | ||||||
en | ||||||
IHI Corporation | ||||||
著者所属(英) | ||||||
en | ||||||
IHI Corporation | ||||||
出版者 | ||||||
出版者 | 日本航空宇宙学会北部支部 | |||||
出版者(英) | ||||||
出版者 | Northern Branch of the Japan Society for Aeronautical and Space Sciences | |||||
書誌情報 |
日本航空宇宙学会北部支部2016年講演会ならびに第17回再使用型宇宙推進系シンポジウム en : JSASS Northern Branch 2016 Annual Meeting and the 17th Symposiun on Propulsion System for Reusable Launch Vehicles 巻 17, 発行日 2016-03 |
|||||
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 | 日本航空宇宙学会北部支部2016年講演会ならびに第17回再使用型宇宙推進系シンポジウム(2016年3月9日-10日. 北海道大学大学院工学研究院), 札幌市, 北海道 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This paper reports the combustion characteristics of LOX/LNG (Liquefied Natural Gas, methane) co-axial type pre-burner injectors under high pressure condition, based on a result of single element firing tests of LOX/methane. LNG rocket engines have been investigated among many countries because LNG has better characteristics as a fuel of rocket engine, i.e. longer storage, lower cost and non-toxic. In Japan, we are conducting research and development on a regenerative cooling LOX/methane engine to achieve higher performance. In order to realize higher performance, LOX and methane have to be mixed and burned with higher efficiency and more stable. Therefore we prepared many single shear coaxial elements which varied design parameters and we performed firing test for the purpose of surveying combustion characteristics of LOX/methane under high pressure condition. The result for all pre-burner elements shows that combustion is stable and generated soot quantity is small. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: CD-ROM1枚 | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Note: One CD-ROM | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA12621350 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AC1600100000 |