高エネルギイオン液体推進剤を用いたレーザ輻射加熱点火式小型スラスタの基礎動作特性の実験評価

Material type: 文書・図像類

Author: 伊東山, 登ほか

Publisher: 宇宙航空研究開発機構(JAXA)

Publication date: 2023-02-03

Material Format: Digital

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Note (General)：: Ammonium dinitramide-based ionic liquid propellants (ADN-EILPs) are expected the candidates with high-performance and low toxicity for next-generation...

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Material Type: 文書・図像類
Title: 高エネルギイオン液体推進剤を用いたレーザ輻射加熱点火式小型スラスタの基礎動作特性の実験評価
Author/Editor: 伊東山, 登
羽生, 宏人
笠原, 次郎
ITOUYAMA, Noboru
HABU, Hiroto
KASAHARA, Jiro
Author Heading: 伊東山, 登
羽生, 宏人
笠原, 次郎
ITOUYAMA, Noboru
HABU, Hiroto
KASAHARA, Jiro
Publication, Distribution, etc.: 宇宙航空研究開発機構(JAXA)
Publication Date: 2023-02-03
Publication Date (W3CDTF): 2023-02-03
Alternative Title: Investigation of Fundamental Operating Characteristics of Laser Radiation Heating Ignited Thrusters Using High-Energetic Ionic Liquid Propellant
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)
No. or year of volume/issue: JAXA-RR-22-006
Volume: JAXA-RR-22-006
Pages: 7-9
ISSN (Periodical Title): ISSN : 2433-2216
Text Language Code: jpn
Subject Heading: Ammonium dinitramide
Ionic liquid
Laser ignition
Small thruster system
Ignition delay
Target Audience: 一般
Note (General): 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
DOI: 10.20637/00049034
Access Restrictions: 限定公開
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