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Combustion wave structure of ADN based composite propellant
https://jaxa.repo.nii.ac.jp/records/2004
https://jaxa.repo.nii.ac.jp/records/2004fd8d4e8f-4a58-4536-9f69-fe1b7019d810
名前 / ファイル | ライセンス | アクション |
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61907001.pdf (664.7 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 | ||||||
言語 | en | |||||
タイトル | Combustion wave structure of ADN based composite propellant | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ADN; burning rate; surface temperature; burning rate modifier; nanoparticle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ADN; burning rate; surface temperature; burning rate modifier; nanoparticle | |||||
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 | |||||
著者 |
Fujisato, Koji
× Fujisato, Koji× Habu, Hiroto× Hori, Keiichi× Shibamoto, Hidefumi× Yu, Xiuchao× Miyake, Atsumi× Fujisato, Koji× Habu, Hiroto× Hori, Keiichi× Shibamoto, Hidefumi× Yu, Xiuchao× Miyake, Atsumi |
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著者所属 | ||||||
東京大学大学院 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
細谷火工株式会社 | ||||||
著者所属 | ||||||
細谷火工株式会社 | ||||||
著者所属 | ||||||
横浜国立大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Graduate School of the University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Hosoya Pyro-Engineering Co., Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Hosoya Pyro-Engineering Co., Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Yokohama National 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24年度研究成果報告書 en : JAXA Research and Development Report: Collaborative Research Activity on Energetic Materials Research Report FY2012 巻 JAXA-RR-12-005, p. 1-7, 発行日 2013-03-29 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Combustion characteristics of pelletized ammonium dinitramide (ADN) and ADN-based propellants have been studied. Micron-meter-sized particles of Al, Fe2O3, TiO2, NiO, Cu(OH)NO3, Cu and CuO, and nano-meter-sized Al (Alex) and CuO (nanoCuO) were employed as the additives for pelletized ADN. Only nanoCuO and Alex show the remarkable effects, so they are also added to ADN-based propellant. The binder of ADN-based propellant is thermoplastic elastomer (TP), and three kinds of mixtures (TP:ADN = 30:70, 20:80 and 10:90 mass%) were prepared .The burning rates of pelletized ADN and ADN-based propellants were measured under the pressure range from 0.6 to 6.2 MPa, and the surface temperature profiles were obtained about ADN-based propellants. Nano-sized CuO enhanced the burning rate of pelletized ADN. Alex-incorporated ADN burned with flames even at 0.55 MPa under which pure ADN does not form the flame. Burning rate of nonadditive ADN-based propellants has extremely high pressure dependency. In the case of TP/ADN (30:7, burning rate jump are found from the critical pressure approximately 3.2MPa. The temperature profiles of TP/ADN (30:70) were measured, and the combustion structure was discussed. Both nanoCuO and Alex improved the burning rate characteristics, and the pressure exponents are 0.54 and 0.76 respectively. | |||||
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: AA0061907001 | |||||
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-12-005 |