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ADN/AN系コンポジット推進薬の着火特性
https://jaxa.repo.nii.ac.jp/records/2047
https://jaxa.repo.nii.ac.jp/records/20475f02d08f-3d24-4992-8742-aa283039e467
名前 / ファイル | ライセンス | アクション |
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65204003.pdf (705.3 kB)
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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/AN系コンポジット推進薬の着火特性 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Solid propellant | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Ammonium dinitramide(ADN) | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Ammonium nitrate(AN) | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Ignition | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Combustion | |||||
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 | Ignition characteristics of ADN/AN composite propellants | |||||
著者 |
松本, 幸太郎
× 松本, 幸太郎× 中臺, 啓太× 生出, 翔× 高橋, 賢一× 桑原, 卓雄× 于, 秀超× 芝本, 秀文× 羽生, 宏人× Matsumoto, Kotaro× Nakadai, Keita× Oide, Sho× Takahashi, Kenichi× Kuwahara, Takuo× Yu, Xiuchao× Shibamoto, Hidefumi× Habu, Hiroto |
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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 | ||||||
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 | ||||||
著者所属 | ||||||
細谷火工 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所宇宙輸送工学研究系 (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 | ||||||
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 | ||||||
著者所属(英) | ||||||
en | ||||||
Hosoya Pyro-Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
Division for Space Propulsion and Propellants, 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報告: 高エネルギー物質研究会: 平成23年度研究成果研究成果報告書 en : JAXA Research and Development Report: Collaborative Research Activity on Energetic Materials Research Report FY2011 巻 JAXA-RR-11-005, p. 25-32, 発行日 2012-03-30 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 本研究では,ADN系推進薬の推進薬表面の燃焼を考察するために,ADNの一部をANに置き換えて着火実験を行った.AN混合量が増加するに従い,着火遅れ時間及び化学的着火遅れ時間が長くなることがわかった.さらに,活性化エネルギーを算出した結果,AN混合量20[mass%]-40[mass%]間で着火特性が変化していることがわかった. | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In this research we obtained ignition delay time, chemical ignition delay time, and activation energy of the Ammonium dinitramide (ADN) / Ammonium nitrate (AN) composite propellants. In the results ignition delay time and chemical ignition delay time decrease with increasing atmosphere temperature and increasing concentration of ADN. Activation energy of ADN/AN composite propellant decrease at concentration of ADN between 40 [mass%] and 60 [mass%]. It is consider that reaction of ADN/AN propellant is changed by increasing concentration of AN. | |||||
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 | 1349-1113 | |||||
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: AA0065204003 | |||||
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-11-005 |