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TG-DSC-HRTOFMSを用いたアンモニウムジニトラミド系イオン液体推進剤の熱-生成ガス同時分析

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TG-DSC-HRTOFMSを用いたアンモニウムジニトラミド系イオン液体推進剤の熱-生成ガス同時分析

Material type
文書・図像類
Author
伊里, 友一朗ほか
Publisher
宇宙航空研究開発機構(JAXA)
Publication date
2019-02-28
Material Format
Digital
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Notes on use

Note (General):

熱重量-示差走査熱-高感度飛行時間型質量複合分析(TG-DSC-HRTOFMS)を用いて,アンモニウムジニトラミド(ADN),モノメチルアンモニウム硝酸塩(MMAN),尿素(urea)から構成される高エネルギーイオン液体推進剤の熱-生成ガス同時分析を行った.本手法は,熱挙動と同時に生成ガスの精密質量...

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Digital

Material Type
文書・図像類
Author/Editor
伊里, 友一朗
塩田, 謙人
佐藤, 健太
佐藤, 孝司
八幡, 行記
羽生, 宏人
三宅, 淳巳
Izato, Yuichiro
Shiota, Kento
Sato, Kenta
Sato, Takashi
Yahata, Yukinori
Habu, Hiroto
Miyake, Atsumi
Publication, Distribution, etc.
Publication Date
2019-02-28
Publication Date (W3CDTF)
2019-02-28
Alternative Title
Thermal and evolved gas analyses of ammonium dinitramide-based ionic propellant using TG-DSC-HRTOFMS
Periodical 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)
No. or year of volume/issue
JAXA-RR-18-006