並列タイトル等Research and Development of Thruster with High Energetic Ionic Liquids for Micro Propulsion System
タイトル（掲載誌）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
一般注記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
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/record/2000214/files/AA2330014001.pdf
連携機関・データベース国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
提供元機関・データベース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