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規格・テクニカルリポート類

高エネルギーイオン液体推進剤を適用した化学スラスタの開発

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高エネルギーイオン液体推進剤を適用した化学スラスタの開発

Material type
規格・テクニカルリポート類
Author
松本, 幸太郎ほか
Publisher
宇宙航空研究開発機構 (JAXA)
Publication date
2024-01-30
Material Format
Digital
Capacity, size, etc.
-
NDC
-
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Note (General):

出版タイプ: VoRAmmonium Dinitramide (ADN)-based ionic liquid propellants are promising new liquid propellants with excellent propulsive performance, stabil...

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Digital

Material Type
規格・テクニカルリポート類
Author/Editor
松本, 幸太郎
勝身, 俊之
伊東山, 登
松永, 浩貴
羽生, 宏人
Publication, Distribution, etc.
Publication Date
2024-01-30
Publication Date (W3CDTF)
2024-01-30
Alternative Title
Development of Chemical Thrusters applying High Energetic Ionic Liquid Propellants
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5年度研究成果報告書
No. or year of volume/issue
JAXA-RR-23-005
Volume
JAXA-RR-23-005
Pages
5-7
ISSN (Periodical Title)
EISSN : 2433-2216
Text Language Code
jpn
Alias of Author
Target Audience
一般
Note (General)
出版タイプ: VoR
Ammonium Dinitramide (ADN)-based ionic liquid propellants are promising new liquid propellants with excellent propulsive performance, stability, and ground handling characteristics. There have been studies on the properties of ADN-based ionic liquids alone and on thruster element technologies such as ignition systems and injectors. Our research group is currently studying chemical thrusters using ADN-based ionic liquids as propellant and is conducting ground burning tests for future space demonstrations. This report summarizes the status of the ground combustion test and the development plan up to the space demonstration.
形態: カラー図版あり
Physical characteristics: Original contains color illustrations
レポート番号:JAXA- RR-23-005
Access Restrictions
インターネット公開
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)
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