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"title": ["AP/HTPB系コンポジット推進薬における粒子間隙に着目したレオロジー特性の評価"], "weko_shared_id": -1}
AP/HTPB系コンポジット推進薬における粒子間隙に着目したレオロジー特性の評価
https://doi.org/10.20637/JAXA-RR-18-006/0007
https://doi.org/10.20637/JAXA-RR-18-006/00076b7789ea-4078-46b2-ae77-eb709ff64bdf
名前 / ファイル | ライセンス | アクション |
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AA1830031007.pdf (1.5 MB)
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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 | 2019-02-28 | |||||
タイトル | ||||||
タイトル | AP/HTPB系コンポジット推進薬における粒子間隙に着目したレオロジー特性の評価 | |||||
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-18-006/0007 | |||||
ID登録タイプ | JaLC | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Evaluation of the rheology of AP/HTPB composite propellant with focus on the gap between particles | |||||
著者 |
寺嶋, 寛成
× 寺嶋, 寛成× 村田, 駿介× 岩崎, 祥大× 羽生, 宏人× 山口, 聡一朗× Terashima, Kansei× Murata, Shunsuke× 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: 平成30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 (2018) 巻 JAXA-RR-18-006, p. 45-48, 発行日 2019-02-28 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 過塩素酸アンモニウム(AP)粒子と末端水酸基ポリブタジエン(HTPB)を主成分とするコンポジット推進薬において,そのレオロジー特性を捉えるために粒子間隙パラメータγを導入する.γの小さな変化に対して推進薬スラリーの形状保持性が大きく変化した.レオロジー特性評価装置を用いて単一粒径で作製した異なるγの値を持つ模擬推進薬の粘弾性を温度別に測定した.特徴的な粒子配置が持つγの値に相当するγ=0.5 から損失弾性率がステップ状に減少した.また,試料温度の上昇に伴い損失弾性率のステップが緩やかになった. | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | We define the gap parameter γ, in order to understand the rheology of AP/HTPB composite propellant. A shape retainability of propellant slurry greatly changes with a slightly change in γ. The viscoelasticity of simulated propellants with different γ was measured using a rheometer at different temperatures. The loss modulus decreased stepwise from γ = 0.5. γ = 0.5 is equivalent to the value of γ of the particle arrangement that particles are in contact with each other in the simple cubic lattice. As the sample temperature rose, the step of loss modulus disappeared. | |||||
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: AA1830031007 | |||||
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-18-006 |