WEKO3
アイテム
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ADN/AN の燃焼速度特性
https://jaxa.repo.nii.ac.jp/records/1972
https://jaxa.repo.nii.ac.jp/records/19729a38371d-f835-4c82-a4aa-6ed6161c0ea8
名前 / ファイル | ライセンス | アクション |
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62089004.pdf (534.9 kB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | ADN/AN の燃焼速度特性 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Ammonium dinitramide | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Ammonium nitrate | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | burning rate | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Solid propellant | |||||
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 | Burning rate characteristics of ADN/AN | |||||
著者 |
松本, 幸太郎
× 松本, 幸太郎× 高橋, 賢一× 桑原, 卓雄× 芝本, 秀文× 羽生, 宏人× Matsumoto, Koutarou× Takahashi, Kenichi× Kuwahara, Takuo× Shibamoto, Hidefumi× Habu, Hiroto |
|||||
著者所属 | ||||||
日本大学理工学部航空宇宙工学科 | ||||||
著者所属 | ||||||
日本大学理工学部航空宇宙工学科 | ||||||
著者所属 | ||||||
日本大学理工学部航空宇宙工学科 | ||||||
著者所属 | ||||||
細谷火工株式会社 | ||||||
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(英) | ||||||
en | ||||||
Department of Aerospace Engineering, College of Science and Technology, Nihon University | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Aerospace Engineering, College of Science and Technology, Nihon University | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Aerospace Engineering, College of Science and Technology, Nihon University | ||||||
著者所属(英) | ||||||
en | ||||||
Hosoya Pyro-Engineering CO., LTD. | ||||||
著者所属(英) | ||||||
en | ||||||
Division for Space Flight Systems, 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(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25年度研究成果報告書 en : JAXA Research and Development Report: Collaborative Research Activity on Energetic Materials Research Report FY2013 巻 JAXA-RR-13-009, p. 31-35, 発行日 2014-03-31 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 本研究ではアンモニウムジニトラミド(ADN)に硝酸アンモニウム(AN)を混合することで,ADN/AN のAN 混合量に対する燃焼速度特性を調べた. その結果,AND/AN の燃焼速度はAN 混合量に比例して減少することがわかった.また, 雰囲気圧力0.1 MPa 及び1 MPa ではAN 混合量10 mass%で約30% 低下し,20 mass%で約50%低下した. 雰囲気圧力2 MPaでは,AN 混合量20 mass%で約40%低下した.雰囲気圧力0.6 MPa 及び1 MPa と比較して2 MPa ではAN 混合量に対する燃焼速度の減少が抑制された. | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | High performance and Low environmental impact is required for the future soli propellants. Many of high energy material (HEMs) compose without halogen atoms. Additionally, the propellants that used HEMs indicate high theoretical propulsion performance through the calculation. Ammonium dinitramide (ADN) is one of the candidates of the new oxidizer for the advanced solid propellant. However, the combustion characteristics of ADN should be understood deeply for the practical use. In this study, the burning rate characteristics of the ADN/AN mixture pellet were investigated to understand the effects of AN mass ratio in the mixture. The results show that the burning rate of the ADN/AN pellet was decreased with increasing the mass ratio of AN in the pellet. Additionally, the burning rate of ADN/AN pellet (AN mass ratio, 20 mass%) was decreased 40 % compared with ADN at 2 MPa. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: 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 illustrations | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-1113 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA1192675X | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0062089004 | |||||
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-13-009 |