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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- 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: VoRAmmonium 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
- DOI
- 10.20637/0002000215
- 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