JAXA Repository / AIREX 未来へ続く、宙(そら)への英知
Other TitleConstruction of detailed chemical reaction model for ADN-EILPs in gas-phase
Author(jpn)伊東山, 登; 伊里, 友一朗; 三宅, 淳巳; 羽生, 宏人
Author(eng)Itoyama, Noboru; Izato, Yuichiro; Miyake, Atsumi; Habu, Hiroto
Author Affiliation(jpn)東京大学 : 日本学術振興会; 横浜国立大学; 横浜国立大学; 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)
Author Affiliation(eng)The University of Tokyo : Japan Society for the Promotion of Science; Yokohama National University; Yokohama National University; Department of Space Flight Systems, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)
Issue Date2019-02-28
Japan Aerospace Exploration Agency (JAXA)
Publication title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30年度研究成果報告書
JAXA Research and Development Report: Technical Report of The Research Activity for High Energy Materials (2018)
Start page33
End page40
Publication date2019-02-28
This study aimed to improve the detailed chemical reaction model of ammonium dinitramide-based deep eutectic ionic liquid in gas-phase. Particularly, dehydrogenations by radical species which weren't included into the conventional model were investigated and added into the conventional model. Their reaction parameters were calculated by ab initio approach. On the sample of ADN:MMAN:urea, its stable combustion wave computed by the modified model showed the good agreement with the experimental result. Reactions related with radical species might be effective for the combustion of ADN:MMAN:urea in gas-phase. On the other hand, calculated results of ADN:MMAN:acetamide and ADN: MEAN:urea were different from experimental results. It was suggested the importance of condense phase reactions in these compositions.
Description形態: カラー図版あり
Physical characteristics: Original contains color illustrations
KeywordsAmmonium Dinitramide; Ionic liquid; detailed chemical reaction; combustion wave
Document TypeTechnical Report
JAXA Category研究開発報告
NASA Subject CategorySpacecraft Propulsion and Power
Report NoJAXA-RR-18-006

Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.