JAXA Repository / AIREX 未来へ続く、宙(そら)への英知
Other TitleStudy on gel propellant of ionic liquid system based on ammonium dinitramide
Author(jpn)塩田, 謙人; 伊里, 友一朗; 松永, 浩貴; 羽生, 宏人; 三宅, 淳巳
Author(eng)Shiota, Kento; Izato, Yuichiro; Matsunaga, Hiroki; Habu, Hiroto; Miyake, Atsumi
Author Affiliation(jpn)横浜国立大学 : 日本学術振興会; 横浜国立大学; 福岡大学; 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); 横浜国立大学
Author Affiliation(eng)Yokohama National University : Japan Society for the Promotion of Science; Yokohama National University; Fukuoka University; Yokohama National University : Department of Space Flight Systems, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS); Yokohama National University
Issue Date2018-01-10
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29年度研究成果報告書
JAXA Research and Development Report: Technical Report of The Research Activity for High Energy Materials (2017)
Start page45
End page49
Publication date2018-01-10
Abstract我々は, ヒドラジンに替わる液体推進剤として, 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系推進剤(EILPs)に着目している. 一方で、液体推進剤と固体推進薬の特長を有する推進剤として期待されるゲル推進剤においても, ヒドラジン誘導体がゲル化する液体推進剤として用いられている. そこで本研究では, ADN 系EILPsのゲル推進剤への適用に向け, ADN 系EILPs からなるイオン液体ゲル推進剤(ILGPs)の調製と熱分析による熱特性の取得を行った. 熱分析には示差走査熱量計(DSC)を用い, ゲル化剤混合による熱挙動への影響を把握した.
Ammonium dinitramide (ADN) based energetic ionic-liquid propellants (EILPs) are expected to be used as replacements of hydrazine derivatives because the derivatives have high toxicity and volatility. For gel propellants (GPs), the propellants have been studied as future propulsion systems. Since GPs use liquid fuels such as hydrazine derivatives, GPs have same problem as liquid propellants. Therefore, we have focused on use the EILPs for ionic liquid gel propellants (ILGPs). Here, ADN based ILGPs were prepared and their thermal analysis of these samples were conducted to obtain a better understanding of their thermal properties.
Description形態: カラー図版あり
Physical characteristics: Original contains color illustrations
KeywordsAmmonium Dinitramide; Energetic Ionic Liquid; Gel Propellants
Document TypeTechnical Report
JAXA Category研究開発報告
NASA Subject CategoryPropellants and Fuels
Report NoJAXA-RR-17-008

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