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AP/HTPB系コンポジット推進薬スラリーにおける動的粘弾性と粒子間隙パラメータの関係
https://doi.org/10.20637/JAXA-RR-19-003/0007
https://doi.org/10.20637/JAXA-RR-19-003/00073c8781b4-b177-4c66-aa5c-01bb798c737b
名前 / ファイル | ライセンス | アクション |
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AA1930018007.pdf (2.9 MB)
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Item type | テクニカルレポート / Technical Report_02(1) | |||||
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公開日 | 2020-02-20 | |||||
タイトル | ||||||
タイトル | AP/HTPB系コンポジット推進薬スラリーにおける動的粘弾性と粒子間隙パラメータの関係 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | AP/HTPB | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | composite propellant | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | rheology | |||||
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 | viscoelasticity | |||||
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 | |||||
ID登録 | ||||||
ID登録 | 10.20637/JAXA-RR-19-003/0007 | |||||
ID登録タイプ | JaLC | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Relation between the dynamic viscoelasticity and gap parameter of AP/HTPB composite propellant slurry | |||||
著者 |
竹下, 雅人
× 竹下, 雅人× 寺嶋, 寛成× 岩崎, 祥大× 羽生, 宏人× 山口, 聡一朗× Takeshita, Masato× Terashima, Kansei× Iwasaki, Akihiro× Habu, Hiroto× Yamaguchi, Soichiro |
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著者所属 | ||||||
関西大学 | ||||||
著者所属 | ||||||
関西大学 | ||||||
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 | ||||||
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 | ||||||
関西大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Kansai University | ||||||
著者所属(英) | ||||||
en | ||||||
Kansai University | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Space Flight Systems, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Space Flight Systems, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Kansai University | ||||||
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: 令和元年度研究成果報告書 en : JAXA Research and Development Report: Technical Report of The Research Activity for High Energy Materials (2019) 巻 JAXA-RR-19-003, p. 41-46, 発行日 2020-02-20 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | AP/HTPBコンポジット推進薬スラリーの粘弾性評価のために粒子間隙パラメータγを導入する.酸化剤の配合比を増やしてAP粒子の粒子間隙γを狭くすると,γ= 0.5前後においてスラリーの動的粘弾性や形状保持性が大きく変化した.この実験結果からAP粒子の稠密な粒子構造体が推進薬全体のレオロジー特性に大きく影響を及ぼす可能性が示唆される. | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | We propose the gap parameter γ between AP particles for viscoelasticity analysis in AP/HTPB composite propellant slurry. When the particle-gap γ of the AP particles was narrowed by increasing the amount of oxidant, the dynamic viscoelasticity and the shape-retaining property changed deeply at around γ = 0.5. This result suggests the possibility that the dense particulate structure of the AP particles greatly contributes to the rheology of the entire slurry. | |||||
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 | |||||
ISSNONLINE | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 2433-2216 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA1930018007 | |||||
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-19-003 |