WEKO3
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アンモニウムジニトラミド系高エネルギー推進剤の最適組成探索手法
https://doi.org/10.20637/JAXA-RR-16-006/0007
https://doi.org/10.20637/JAXA-RR-16-006/0007abf04cfe-07ca-4385-a5a4-b25d97da99d1
名前 / ファイル | ライセンス | アクション |
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AA1630043007.pdf (894.3 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 | 2017-03-23 | |||||
タイトル | ||||||
タイトル | アンモニウムジニトラミド系高エネルギー推進剤の最適組成探索手法 | |||||
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 | melting point prediction | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | CALPHAD method | |||||
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-16-006/0007 | |||||
ID登録タイプ | JaLC | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Searching method of optimum composition ratio for ADN-based ionic liquids propellants | |||||
著者 |
塩田, 謙人
× 塩田, 謙人× 早田, 葵× 板倉, 正昂× 伊里, 友一朗× 松永, 浩貴× 羽生, 宏人× 三宅, 淳巳× Shiota, Kento× Hayata, Mamoru× Itakura, Masataka× Izato, Yuichiro× Matsunaga, Hiroki× Habu, Hiroto× Miyake, Atsumi |
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著者所属 | ||||||
横浜国立大学 : 日本学術振興会 | ||||||
著者所属 | ||||||
横浜国立大学 | ||||||
著者所属 | ||||||
横浜国立大学 | ||||||
著者所属 | ||||||
横浜国立大学 | ||||||
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) | ||||||
著者所属 | ||||||
横浜国立大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Yokohama National University : Japan Society for the Promotion of Science | ||||||
著者所属(英) | ||||||
en | ||||||
Yokohama National University | ||||||
著者所属(英) | ||||||
en | ||||||
Yokohama National University | ||||||
著者所属(英) | ||||||
en | ||||||
Yokohama National University | ||||||
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) | ||||||
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28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 (2016) 巻 JAXA-RR-16-006, p. 47-51, 発行日 2017-03-10 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | アンモニウムジニトラミド(ADN)から構成される高エネルギーイオン液体推進剤(EILPs) は, 構成成分の混合による共融現象の融点降下を利用した液体である. そのため, EILPsの構成成分や組成比を変化させることで, 推進剤の融点や性能のデザインが可能である. 一方で, その組み合わせが膨大であるため構成成分を決定した後に, 十分な燃焼性能と運用可能な融点を有するバランスの取れた組成比探索のスクリーニング手法が必要となる.そこで本研究では, ADN系EILPs(ADN-EILPs)の最適組成探索手法の提案を目的とし, 任意の組成比における融点予測結果と比推力の計算結果を三角組成図にマッピングした. その結果, 熱分析データから算出した融点予測結果は, 実測値と良い相関を示し, 三角図から最適組成探索に向けたスクリーニングが可能となった. | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Energetic ionic-liquid propellants (EILPs) are expected as liquid rocket propellant for next generation. We focus on EILPs which are made of deep eutectic ionic liquid. We selected ammonium nitrate (ADN) based EILPs (ADN-EILPs) for model EILPs. ADN is high energetic material. Melting point of ADN is 92 C. The low melting point is suitable for preparation the EILPs. Preparation of the EILPs is easier than other EILPs. Performance and melting point of the EILPs depend on mixing ratio of EILPs component. It is necessary to predict ideal mixing ratio the EILPs which have competent performance and melting point for efficient EILPs design. In this paper, we show screening method for searching compositions of the EILPs on thermal analysis. | |||||
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: AA1630043007 | |||||
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-16-006 |