超小型衛星を見据えた高エネルギーイオン液体推進系の研究開発

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: 2024-01-30

Material Format: Digital

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Note (General)：: We are conducting research and development of chemical propulsion systems for satellites using ammonium dinitramide (ADN)-based energetic ionic liquid...

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Material Type: 文書・図像類
Title: 超小型衛星を見据えた高エネルギーイオン液体推進系の研究開発
Author/Editor: 松永, 浩貴
伊東山, 登
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
Author Heading: 松永, 浩貴
伊東山, 登
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
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: Research and Development of Thruster with High Energetic Ionic Liquids for Micro Propulsion System
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: 1-4
ISSN (Periodical Title): EISSN : 2433-2216
Text Language Code: jpn
Alias of Author: ITOYAMA, Noboru
IZATO, Yuichiro
Subject Heading: Monopropellant
Thruster
Micro Propulsion System
High Energetic Materials
Ionic Liquid
Target Audience: 一般
Note (General): We are conducting research and development of chemical propulsion systems for satellites using ammonium dinitramide (ADN)-based energetic ionic liquids (EILs) as propellants. They are expected to be used as propellants for high-performance and safe nano-satellite propulsion systems. The project aims to demonstrate the EILs in orbit within a few years, and this year, in parallel with the development of new thruster systems using laser and electrolytic ignition, and the advancement of new EILs-specific technologies such as the design of highly reactive ADN-based EILs, a prototype thruster using a simple method was built and a ground combustion test was conducted. The thruster has been tested in ground combustion tests. In the future, we plan to demonstrate the thruster's propulsion performance to clarify its feasibility as a chemical propulsion system, and then proceed with the fabrication of a thruster equipped with each new technology.
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: 10.20637/0002000214
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