JAXA Repository / AIREX 未来へ続く、宙(そら)への英知
64905002.pdf1.25 MB
Other TitleStudy of ADN-based Solid Propellant
Author(jpn)藤里, 公司; 羽生, 宏人; 三宅, 淳巳; 堀, 恵一
Author(eng)Fujisato, Koji; Habu, Hiroto; Miyake, Atsumi; Hori, Keiichi
Author Affiliation(jpn)東京大学大学院工学研究科; 宇宙航空研究開発機構宇宙科学研究所; 横浜国立大学大学院環境情報学府; 宇宙航空研究開発機構宇宙科学研究所
Author Affiliation(eng)Graduate School of Engineering, University of Tokyo; Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS); Graduate School of Environment and Information Sciences, Yokohama National University; Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)
Issue Date2011-03-01
PublisherJapan Aerospace Exploration Agency (JAXA)
Publication titleJAXA research and development memorandum
宇宙航空研究開発機構研究開発資料: 高エネルギー物質研究会研究成果報告書
Publication date2011-03-01
AbstractFor the development of green solid propellants with high combustion performance, the composition should be replaced with high energy materials. In this research, Ammonium dinitramide (ADN) was studied to improve the solid rocket motor performance as an oxidizer. The synthesis process of ADN was investigated with the method which has been reported and the crystal shape of products was modified to the spherical to enhance the mass ratio of the oxidizer in solid propellant. This paper reports the results of the experimental estimation of the combustion characteristics of the propellant with ADN include the chemical properties of it.
高性能・低環境負荷の固体推進薬を開発するには,推進薬の組成から見直す必要がある.本研究では高エネルギー酸化剤のひとつであるアンモニウムジニトラミド(ADN)を用いたコンポジット推進薬の検討を行った.ADN の合成方法,粒子形状の制御方法,バインダの選定および混練,ストランド燃焼実験について実験を行い 具体的な設計指針を得た.
DescriptionOriginal contains color illustrations
形態: カラー図版あり
KeywordsSolid propellant; Ammonium dinitramide (AND); Synthesis; Burning rate
Document TypeTechnical Report
JAXA Category研究開発資料
Report NoJAXA-RM-10-015

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