WEKO3
アイテム
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低毒性推進剤による二液式推進系の研究開発
https://jaxa.repo.nii.ac.jp/records/16592
https://jaxa.repo.nii.ac.jp/records/165924489f3fd-9f8c-4fe2-9ba6-b9cbd91e48be
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 低毒性推進剤による二液式推進系の研究開発 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Propulsion,Bi-Propellant,Green Propellant,Microsatellite | |||||
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 | Research of Bi-Propellant System Based on Green Propellant | |||||
著者 |
鈴木, 信義
× 鈴木, 信義× 佐原, 宏典× Suzuki, Nobuyoshi× Sahara, Hironori |
|||||
著者所属 | ||||||
首都大学東京システムデザイン学部 | ||||||
著者所属 | ||||||
首都大学東京システムデザイン学部 | ||||||
著者所属(英) | ||||||
en | ||||||
Faculty of System Design, Tokyo Metropolitan University | ||||||
著者所属(英) | ||||||
en | ||||||
Faculty of System Design, Tokyo Metropolitan University | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究本部 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙輸送シンポジウム: 講演集録 en : Proceedings of Space Transportation Symposium 巻 平成21年度, 発行日 2010-01 |
|||||
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 | 平成21年度宇宙輸送シンポジウム(2010年1月14日-15日, 宇宙航空研究開発機構宇宙科学研究本部) | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Space Transportation Symposium (January 14-15, 2010. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)), Sagamihara, Kanagawa Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | We have been studying the generalized propulsion system based on green mono/bi-propellant since 2008. While, the last achievements prove feasibility of the propulsion system and conducted captive test with a breadboard model (BBM), no ignition was confirmed there. Accordingly, we modified the ejector in thruster and measured droplet diameter of liquid propellant in combustion chamber, and improved performance of propellant atomization. | |||||
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 | AN10324301 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0064741022 |