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高エネルギーイオン液体推進剤の点火に関する検討
https://doi.org/10.20637/JAXA-RR-17-008/0001
https://doi.org/10.20637/JAXA-RR-17-008/00019a6dd3c4-3370-46f3-995e-56df53df641f
名前 / ファイル | ライセンス | アクション |
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AA1730012001.pdf (1.1 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 | 2018-02-06 | |||||
タイトル | ||||||
タイトル | 高エネルギーイオン液体推進剤の点火に関する検討 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Energetic Ionic Liquid Propellants (EILPs) | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | High Energetic Materials | |||||
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 | Thruster | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Laser Ignition | |||||
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-17-008/0001 | |||||
ID登録タイプ | JaLC | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Study for ignition of high energy ionic liquid propellant | |||||
著者 |
松永, 浩貴
× 松永, 浩貴× 羽生, 宏人× 野田, 賢× 三宅, 淳巳× Matsunaga, Hiroki× Habu, Hiroto× Noda, Masaru× Miyake, Atsumi |
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著者所属 | ||||||
福岡大学 | ||||||
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) : 横浜国立大学 | ||||||
著者所属 | ||||||
福岡大学 | ||||||
著者所属 | ||||||
横浜国立大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Fukuoka University | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Space Flight Systems, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) : Yokohama National University | ||||||
著者所属(英) | ||||||
en | ||||||
Fukuoka University | ||||||
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29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 (2017) 巻 JAXA-RR-17-008, p. 1-6, 発行日 2018-01-10 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 我々は高エネルギー物質を基剤新規液体の推進薬の研究開発を進めている. 固体エネルギー物質同士の共融により調製されるイオン液体推進剤(EILPs)は溶媒を含まず低揮発性であることから, 高性能低毒性推進剤として期待できる. 点火手法はEILPs の実用化に向けて最も重要な課題のひとつであり, 新規手法としてレーザー点火に着目し, 検討を行っている. 本研究では高エネルギー物質であるアンモニウムジニトラミド(ADN)を基剤としたEILPs が加熱により点火するための条件を把握するため, 熱分解に伴う温度や生成ガスを測定した. | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | We have been studying a new rocket propellant for a thruster based on high energetic materials in order to replace of hydrazine. Energetic ionic liquid propellants (EILPs) which is eutectic mixture of solid energetic materials are expected to have high energy and low toxicity because EILPs are solvent-free and low-volatility liquid. Ignition method is one of the most problems for realization of EILPs. We are studying laser ignition as new ignition method. In this study, to understand condition for ignition of ammonium dinitramide (ADN)-based EILPs by heating, temperature and gas product during thermal decomposition were measured. | |||||
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: AA1730012001 | |||||
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-17-008 |