@techreport{oai:jaxa.repo.nii.ac.jp:00046289,
 author = {塩田, 謙人 and 松下, 和樹 and 伊里, 友一朗 and 三宅, 淳巳 and Shiota, Kento and Matsushita, Kazuki and Izato, Yuichiro and Miyake, Atsumi},
 month = {Feb},
 note = {高エネルギー物質研究会ではアンモニウムジニトラミド(ADN)を主な構成成分とした共融現象を利用した高エネルギーイオン液体系推進剤(EILPs)の研究を進めてきた．現行の候補組成は高密度，低融点などの特徴がある一方で着火に課題を有する．課題の解決には新規着火システムおよび新規組成の提案が挙げられる．本検討ではADN系EILPsの新規構成成分として2-ヒドロキシエチルヒドラジニウム硝酸塩(HEHN ，[HOH2CH2CNH2NH2](+)NO3(-))に着目した．HEHN はアメリカ空軍が研究開発している推進剤の主成分として用いられている．しかし，HEHN 単体の熱特性に関する報告例は少ない．そこで，本研究ではHEHNの基礎的な熱特性の取得を目的とし，HEHNの熱分析および生成ガス分析を行い熱挙動および発生するガス種を特定した．, Our research group has focused on energetic ionic-liquid propellants (EILPs) using energetic material such as ammonium dinitramide liquefied without solvents. 2-hydroxyethylhydrazinium nitrate (HEHN) is liquid and has a glass transition at -56.9 C. It is expected that HEHN is used as a eutectic composition to develop EILPs. The United States Air Force Research Laboratory has developed the liquid propellant consisting of hydroxyl ammonium nitrate and HEHN. For the development and use of EILPs with HEHN, understanding of the thermal properties of the compound containing HEHN is essential. On the other hand, little has been reported on the thermal properties of HEHN. Therefore, the objective of the present study was to obtain a better understanding of the thermal properties of HEHN. This study conducted thermal analysis and evolved gas analysis. From the results, thermal behavior and as species evolved formed from thermal decomposition were identified., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA1930018003, レポート番号: JAXA-RR-19-003},
 title = {2-ヒドロキシエチルヒドラジニウム硝酸塩の基礎的熱特性の把握},
 year = {2020}
}