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Regression Rate Measurement of Hybrid Rocket Using Ultrasonic's
https://jaxa.repo.nii.ac.jp/records/16205
https://jaxa.repo.nii.ac.jp/records/16205ffc076cf-e89e-4c94-b47b-ceece8987d04
名前 / ファイル | ライセンス | アクション |
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61856069.pdf (661.3 kB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Regression Rate Measurement of Hybrid Rocket Using Ultrasonic's | |||||
言語 | ||||||
言語 | eng | |||||
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 | |||||
著者 |
Chang, Po-Jul
× Chang, Po-Jul× 和田, 豊× 勝身, 俊之× 堀, 恵一× 中山, 秀夫× 木村, 元康× Chang, Po-Jul× Wada, Yutaka× Katsumi, Toshiyuki× Hori, Keiichi× Nakayama, Hideo× Kimura, Motoyasu |
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著者所属 | ||||||
東京大学 | ||||||
著者所属 | ||||||
秋田大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS) | ||||||
著者所属 | ||||||
株式会社IHIエアロスペース | ||||||
著者所属 | ||||||
日油株式会社 | ||||||
著者所属(英) | ||||||
en | ||||||
The University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Akita University | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
IHI AEROSPACE Co. Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
NOF Corporation | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS) | |||||
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24年度宇宙輸送シンポジウム: 講演集録 en : Proceedings of Space Transportation Symposium: FY2012 発行日 2013-01 |
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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24年度宇宙輸送シンポジウム (2013年1月17日-1月18日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)), 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 FY2012 (January 17-18, 2013. 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 | A lab-scale hybrid motor burning test was conducted to investigate the solid-fuel regression rate. Real time ultrasonic sensors were used to determine the instantaneous and local burning rate. Polyethylene Glycol (PEG) was chosen as a hybrid rocket fuel. PEG is interest since PEG copolymerizes and mixes well with Glycidyl Azide Polymer (GAP) which is one of the top-rated candidates for next generation hybrid motor, and PEG works as a diluent material to depression the unusual high burning rate of GAP. | |||||
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: PDF | |||||
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 | Physical characteristics: PDF | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0061856069 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: STCP-2012-069 |