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人工筋肉アクチュエータによる固体推進薬の捏和
https://jaxa.repo.nii.ac.jp/records/1939
https://jaxa.repo.nii.ac.jp/records/1939cb8ed0fd-d835-4302-be52-1ebb8f6c8d21
名前 / ファイル | ライセンス | アクション |
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-04-10 | |||||
タイトル | ||||||
タイトル | 人工筋肉アクチュエータによる固体推進薬の捏和 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Solid Rocket Propellant | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Mixing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Slurry | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Artificial Muscle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Peristaltic Pump | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | The mixing of solid propellant by an artificial muscle actuator | |||||
著者 |
岩崎, 祥大
× 岩崎, 祥大× 伴, 遼介× 吉浜, 舜× 中村, 太郎× 羽生, 宏人× Iwasaki, Akihiro× Ban, Ryosuke× Yoshihama, Shun× Nakamura, Taro× Habu, Hiroto |
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著者所属 | ||||||
総合研究大学院大学 | ||||||
著者所属 | ||||||
中央大学 | ||||||
著者所属 | ||||||
中央大学 | ||||||
著者所属 | ||||||
中央大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所宇宙飛翔工学研究系(JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
The Graduate University for Advanced Studies (SOKENDAI) | ||||||
著者所属(英) | ||||||
en | ||||||
Chuo University | ||||||
著者所属(英) | ||||||
en | ||||||
Chuo University | ||||||
著者所属(英) | ||||||
en | ||||||
Chuo University | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Space Flight Systems, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構(JAXA) | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構研究開発報告: 高エネルギー物質研究会: 平成26年度研究成果報告書 en : JAXA Research and Development Report 巻 JAXA-RR-14-005, p. 41-47, 発行日 2015-03-13 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 本研究は固体ロケットの製造プロセスからの抜本的な低コスト化を目標としている.その低コスト化へ繋がるアイデアとしてプロセスの連続プロセス化を目指し,特に固体ロケット推進薬捏和工程に注目した.捏和機に蠕動運動ポンプを用いることでロケット推進薬スラリの流動性を用いた捏和が可能となるだけでなく,安全な捏和を行うことができる. | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This research aims to reduce the cost of the solid rocket motor production, mainly solid propellant. The production process of the solid rocket propellant are usually employed the multi-batch mixing. However, this study using a peristaltic pump as a mixer will lead to the continuous process. The pump system can mix the powder materials for propellant and we consider that it will make the slurry of the solid propellant efficiently by the mechanism of the fluid dynamics in the pump. | |||||
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 | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-1113 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA1192675X | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA1530013006 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-RR-14-005 |