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高エネルギイオン液体推進剤の小型スラスタ概念設計
https://doi.org/10.20637/00048269
https://doi.org/10.20637/000482698baa9ce7-0b25-4bfa-8e8f-34a997eafa91
名前 / ファイル | ライセンス | アクション |
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AA2130019002.pdf (1.2 MB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2022-02-04 | |||||
タイトル | ||||||
タイトル | 高エネルギイオン液体推進剤の小型スラスタ概念設計 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Ammonium dinitramide | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Ionic liquid | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Laser ignition | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Small thruster system | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
ID登録 | ||||||
ID登録 | 10.20637/00048269 | |||||
ID登録タイプ | JaLC | |||||
その他のタイトル(英) | ||||||
その他のタイトル | A Concept of the Small Chemical Thruster with High Energetic Ionic Liquids | |||||
著者 |
伊東山, 登
× 伊東山, 登× 和田, 明哲× 羽生, 宏人× ITOUYAMA, Noboru× WADA, Asato× HABU, Hiroto |
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著者所属 | ||||||
名古屋大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所宇宙飛翔工学研究系(JAXA)(ISAS) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所宇宙飛翔工学研究系(JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Nagoya University | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Space Flight Systems, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Space Flight Systems, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構(JAXA) | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
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3年度研究成果報告書 en : JAXA Research and Development Report: Technical Report of The Research Activity for High Energy Materials (2021) 巻 JAXA-RR-21-002, p. 6-8, 発行日 2022-02-04 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | アンモニウムジニトラミドを基材とするイオン液体系推進剤 (ADN-EILPs) は,低毒・高密度比推力が期待される有望な一液推進剤の一つである.これまで筆者らは,ADN-EILPs が内包する点火・着火特性に関連する技術課題の克服に取り組んできた.昨今の研究により,新たな点火方式として,レーザ輻射加熱機構とレーザ吸光材の組み合わせを考案し, ADN-EILPs の効果的な点火の糸口を見出すまでに至った.本報告では,これら点火に関連する研究の展開として,当該点火機構に新たな推進剤供給機構を組み合わせた,ADN-EILPs を用いるスラスタの概念について紹介する. | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Ammonium dinitramide-based ionic liquid propellants (ADN-EILPs) are expected the candidates with high-performance and low toxicity for next-generation chemical thruster in small satellites. Authors have investigated the ignition of ADN-EILPs to solve technical problems for thruster applications, e.g. ignitor or ignition mechanism of ADN-EILPs. Through the past studies, the combination of laser radiant heating and carbon-based laser absorbent was found out as a solution of expected ignition methods for ADN-EILPs. This paper introduces a thruster concept using ADN-EILPs by utilizing the new propellant supply method as well as such the ignition mechanism. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
ISSNONLINE | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 2433-2216 | |||||
著者版フラグ | ||||||
出版タイプ | VoR | |||||
出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA2130019002 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-RR-21-002 |