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次世代固体ロケット用低融点熱可塑性推進薬のアルミ添加による高性能化
https://jaxa.repo.nii.ac.jp/records/16493
https://jaxa.repo.nii.ac.jp/records/16493732b6b7b-d4f0-4f5f-bce9-9b4fb3953a9d
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 | 次世代固体ロケット用低融点熱可塑性推進薬のアルミ添加による高性能化 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | LTP | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Low Melting Temperature Thermoplastic Propellant | |||||
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 | The Development of Low Melting Temperature Thermoplastic Propellant (LTP) with Aluminum Addition for the Next Generation Solid Rocket | |||||
著者 |
高田, 淳史
× 高田, 淳史× 福地, 亜宝郎× 松浦, 新× 宮川, 清× 岡本, 久夫× Takada, Atsushi× Fukuchi, Aporo× Matsuura, Shin× Miyakawa, Kiyoshi× Okamoto, Hisao |
|||||
著者所属 | ||||||
IHIエアロスペース | ||||||
著者所属 | ||||||
IHI Aerospace (IA) | ||||||
著者所属 | ||||||
IHIエアロスペース | ||||||
著者所属 | ||||||
IHIエアロスペース | ||||||
著者所属 | ||||||
IHIエアロスペース・エンジニアリング | ||||||
著者所属(英) | ||||||
en | ||||||
IHI Aerospace (IA) | ||||||
著者所属(英) | ||||||
en | ||||||
IHI Aerospace | ||||||
著者所属(英) | ||||||
en | ||||||
IHI Aerospace (IA) | ||||||
著者所属(英) | ||||||
en | ||||||
IHI Aerospace (IA) | ||||||
著者所属(英) | ||||||
en | ||||||
IHI Aerospace Engineering | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究所 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | |||||
書誌情報 |
平成22年度宇宙輸送シンポジウム: 講演集録 en : Proceedings of Space Transportation Symposium: FY2010 発行日 2011 |
|||||
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22年度宇宙輸送シンポジウム(2011年1月20-21日. 宇宙航空研究開発機構宇宙科学研究所), 相模原市, 神奈川県 | |||||
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 FY2010 (January 20-21, 2011. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)), Sagamihara, Kanagawa Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Authors have developed low melting temperature thermoplastic propellant (LTP) for the Next Generation Solid Rocket by using thermoplastic elastomer. For more improvement performance, aluminum (Al) addition to LTP was studied. They produced LTP with Al addition experimentally, which productivity, mechanical properties, and combustion properties were obtained. Al less than 16% and binder more than 18% were necessary to mixing and fusion molding. Regarding mentioned properties, best composition (Binder/AP/Al=18/66/16) was selected in this study. | |||||
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: AA0065073046 |