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: 文書・図像類

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

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Note (General)：: Ammonium Dinitramide (ADN)-based ionic liquid propellants are promising new liquid propellants with excellent propulsive performance, stability, and g...

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Material Type: 文書・図像類
Title: 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
Author/Editor: 松本, 幸太郎
勝身, 俊之
伊東山, 登
松永, 浩貴
羽生, 宏人
Author Heading: 松本, 幸太郎
勝身, 俊之
伊東山, 登
松永, 浩貴
羽生, 宏人
Publication, Distribution, etc.: 宇宙航空研究開発機構 (JAXA)
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: ITOYAMA, Noboru
Subject Heading: Liquid Propellant
Ionic Liquid
High Energetic Material
Chemical Propulsion
Target Audience: 一般
Note (General): 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
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）
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