並列タイトル等Investigation of Fundamental Operating Characteristics of Laser Radiation Heating Ignited Thrusters Using High-Energetic Ionic Liquid Propellant
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4年度研究成果報告書 = JAXA Research and Development Report: Technical Report of The Research Activity for High Energy Materials (2022)
一般注記Ammonium dinitramide-based ionic liquid propellants (ADN-EILPs) are expected the candidates with high-performance and low toxicity for next-generation chemical thrusters in small satellites. Through past studies, authors have investigated the laser radiant heating ignition of ADN-EILPs to solve technical problems for thruster applications and proposed a thruster concept using ADN-EILPs by utilizing the new propellant supply method as well as such the ignition mechanism. From a new hot-fire test following the previous ones, this paper describes the recent result and discussion about the operational properties of composed thruster based on the concept.
形態: カラー図版あり
Physical characteristics: Original contains color illustrations
資料番号: AA2230017002
レポート番号: JAXA-RR-22-006
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=49051&item_no=1&attribute_id=31&file_no=1
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