WEKO3
アイテム
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小型有翼ロケット実験機(WIRES#015)への搭載を想定したLOX/LNG(メタン)エンジンの概念検討
https://jaxa.repo.nii.ac.jp/records/38806
https://jaxa.repo.nii.ac.jp/records/38806720b15ad-995d-4366-a408-32ac09160f23
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 | 小型有翼ロケット実験機(WIRES#015)への搭載を想定したLOX/LNG(メタン)エンジンの概念検討 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | LOX | |||||
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 | LNG | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Liquid rocket engine | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Reusable Launch Vehicle | |||||
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 | Conceptual study on LOX/LNG(methane) engine for WIRES#015 (WInged REusable Sounding rocket) | |||||
著者 |
淺川, 弘也
× 淺川, 弘也× 南里, 秀明× 増田, 井出夫× 石本, 真二× 井上, 琢磨× 石原, 新史× 石崎, 真一郎× 米本, 浩一× Asakawa, Hiroya× Nanri, Hideaki× Masuda, Ideo× Ishimoto, Shinji× Inoue, Takuma× Ishihara, Shinji× Ishizaki, Shinichiro× Yonemoto, Koichi |
|||||
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 | ||||||
株式会社IHIエアロスペース | ||||||
著者所属 | ||||||
株式会社IHIエアロスペース | ||||||
著者所属 | ||||||
株式会社IHI | ||||||
著者所属 | ||||||
九州工業大学 | ||||||
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 | ||||||
IHI AEROSPACE Co., Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
IHI AEROSPACE Co., Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
IHI Corporation | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu Institute of Technology | ||||||
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59回宇宙科学技術連合講演会講演集 en : Proceedings of 59th Space Sciences and Technology Conference 発行日 2015-10-07 |
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関係URI | ||||||
識別子タイプ | URI | |||||
関連識別子 | https://www.jsass.jp/conference/sstc59.php | |||||
関連名称 | https://www.jsass.jp/conference/sstc59.php | |||||
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59回宇宙科学技術連合講演会(2015年10月7日-14日. かごしま県民交流センター), 鹿児島市, 鹿児島 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This paper reports the result of conceptual study on LOX/LNG(methane) engine for WIRES#015 (WInged Reusable Sounding rocket). LNG has better characteristics for rocket fuel, i.e. longer storage, lower cost and non-toxic. In particular, when applying LNG engine for booster stage of reusable launch vehicle (RLV), the vehicle size can be smaller and fuel cost can be reduced. Therefore, we have been studying on LNG engine for RLV. As part of this study, we plan to apply LNG engine to WIRES#015 and perform flight experiment to identify the challenges of LNG engine for RLV. | |||||
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(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11800503 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AC1600075000 | |||||
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-2015-4250 |