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ADN系固体推進薬に関する研究
https://jaxa.repo.nii.ac.jp/records/2561
https://jaxa.repo.nii.ac.jp/records/2561d2c23742-faa6-4f23-918d-ae9e650f6700
名前 / ファイル | ライセンス | アクション |
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64905002.pdf (1.3 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 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | ADN系固体推進薬に関する研究 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Solid propellant; Ammonium dinitramide (AND); Synthesis; Burning rate | |||||
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 | Study of ADN-based Solid Propellant | |||||
著者 |
藤里, 公司
× 藤里, 公司× 羽生, 宏人× 三宅, 淳巳× 堀, 恵一× Fujisato, Koji× Habu, Hiroto× Miyake, Atsumi× Hori, Keiichi |
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著者所属 | ||||||
東京大学大学院工学研究科 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所 | ||||||
著者所属 | ||||||
横浜国立大学大学院環境情報学府 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
Graduate School of Engineering, University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Graduate School of Environment and Information Sciences, Yokohama National University | ||||||
著者所属(英) | ||||||
en | ||||||
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 | |||||
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資料: 高エネルギー物質研究会研究成果報告書 en : JAXA Research and Development Memorandum 巻 JAXA-RM-10-015, 発行日 2011-03-01 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 高性能・低環境負荷の固体推進薬を開発するには,推進薬の組成から見直す必要がある.本研究では高エネルギー酸化剤のひとつであるアンモニウムジニトラミド(ADN)を用いたコンポジット推進薬の検討を行った.ADN の合成方法,粒子形状の制御方法,バインダの選定および混練,ストランド燃焼実験について実験を行い 具体的な設計指針を得た. | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | For the development of green solid propellants with high combustion performance, the composition should be replaced with high energy materials. In this research, Ammonium dinitramide (ADN) was studied to improve the solid rocket motor performance as an oxidizer. The synthesis process of ADN was investigated with the method which has been reported and the crystal shape of products was modified to the spherical to enhance the mass ratio of the oxidizer in solid propellant. This paper reports the results of the experimental estimation of the combustion characteristics of the propellant with ADN include the chemical properties of it. | |||||
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 | 1349-1121 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11983593 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0064905002 | |||||
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-RM-10-015 |