将来宇宙利用に向けた高エネルギーイオン液体推進剤の研究

Material type: 文書・図像類

Author: 松永, 浩貴ほか

Publisher: 宇宙航空研究開発機構(JAXA)

Publication date: 2021-02-10

Material Format: Digital

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Note (General)：: The development of microsatellite is important for expansion of space utilization. The ''energetic ionic liquids (EILs)'', eutectic liquids of high en...

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Material Type: 文書・図像類
Title: 将来宇宙利用に向けた高エネルギーイオン液体推進剤の研究
Author/Editor: 松永, 浩貴
伊東山, 登
和田, 明哲
松本, 幸太郎
塩田, 謙人
伊里, 友一朗
勝身, 俊之
羽生, 宏人
野田, 賢
三宅, 淳巳
MATSUNAGA, Hiroki
ITOUYAMA, Noboru
WADA, Asato
MATSUMOTO, Kotaro
SHIOTA, Kento
IZATO, Yuichiro
KATSUMI, Toshiyuki
HABU, Hiroto
NODA, Masaru
MIYAKE, Atsumi
Author Heading: 松永, 浩貴
伊東山, 登
和田, 明哲
松本, 幸太郎
塩田, 謙人
伊里, 友一朗
勝身, 俊之
羽生, 宏人
野田, 賢
三宅, 淳巳
MATSUNAGA, Hiroki
ITOUYAMA, Noboru
WADA, Asato
MATSUMOTO, Kotaro
SHIOTA, Kento
IZATO, Yuichiro
KATSUMI, Toshiyuki
HABU, Hiroto
NODA, Masaru
MIYAKE, Atsumi
Publication, Distribution, etc.: 宇宙航空研究開発機構(JAXA)
Publication Date: 2021-02-10
Publication Date (W3CDTF): 2021-02-10
Alternative Title: Research of High Energetic Ionic Liquid Propellants for Future Space Applications
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: 令和2年度研究成果報告書 = JAXA Research and Development Report: Technical Report of The Research Activity for High Energy Materials (2020)
No. or year of volume/issue: JAXA-RR-20-007
Volume: JAXA-RR-20-007
Pages: 1-4
ISSN (Periodical Title): ISSN : 2433-2216
Text Language Code: jpn
Subject Heading: Monopropellant
Thruster
Micro Propulsion System
High Energetic Materials
Ionic Liquid
Target Audience: 一般
Note (General): The development of microsatellite is important for expansion of space utilization. The ''energetic ionic liquids (EILs)'', eutectic liquids of high energetic materials, are promising new liquid propellant replacing hydrazine because their unique properties, high energy density, low vapor pressure, enable miniaturization of system, easier handling, and reduction of explosion risks. The mixture of ammonium dinitramide (ADN), monomethylamine nitrate (MMAN), and urea forms EILs and it is one of the candidate for new propellant. To realize the on-orbit demonstration of propulsion systems using EILs within several years, we are advancing researches of component technology; synthesis with highly safety and low cost, propulsion system using laser ignition and electrical energy, and risk assessment for safety use from design to operation.
形態: カラー図版あり
Physical characteristics: Original contains color illustrations
資料番号: AA2030016001
レポート番号: JAXA-RR-20-007
DOI: 10.20637/00047347
Access Restrictions: 限定公開
Data Provider (Database): 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
https://irdb.nii.ac.jp
Original Data Provider (Database): 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ