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Development of gas-liquid equilibrium thruster for small satellite
https://jaxa.repo.nii.ac.jp/records/7522
https://jaxa.repo.nii.ac.jp/records/7522c73894e3-08d5-4000-897e-015aa65cef21
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Development of gas-liquid equilibrium thruster for small satellite | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 気液平衡スタスタ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | SSSAT | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 小型ソーラーセイル衛星 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 能動ニューテーション制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ANC | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 燃料噴射 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | イソブタン | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 化学反応制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 推力 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道変換 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 姿勢制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | バルブ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ノズル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 小型衛星技術 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙機推進 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | gas-liquid equilibrium thruster | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | SSSAT | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Small Solar Sail Satellite | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Active Nutation Control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ANC | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | fuel injection | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | isobutene | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | chemical reaction control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | thrust | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | orbital maneuver | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | attitude control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | valve | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | nozzle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | small satellite technology | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spacecraft propulsion | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
その他のタイトル | ||||||
その他のタイトル | 小型衛星用気液平衡スラスタの開発 | |||||
著者 |
山本, 高行
× 山本, 高行× 森, 治× 志田, 真樹× Yamamoto, Takayuki× Mori, Osamu× Shida, Maki |
|||||
著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究本部 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS) | |||||
書誌情報 |
第16回アストロダイナミクスシンポジウム講演後刷り集 2006 en : Proceedings of 16th Workshop on JAXA Astrodynamics and Flight Mechanics p. 117-120, 発行日 2007-03 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 小型衛星においても、能動的な制御により、姿勢変更あるいは軌道変更を行うことがミッションとして要求されうる。小型衛星の姿勢制御および軌道遷移のためのスラスタシステムには、小型・軽量であり、取り扱いの容易な燃料を用いることが要求される。本研究では燃料として取り扱いの比較的容易なイソブタンを用いることで、イソブタンの気液平衡を利用した蒸気圧による燃料噴射システムを構築する。小型衛星に特化した推進系として良好な特性が得られたことを、実験を通して示す。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The small satellite, demonstrating the power generation by film solar cell of solar sail, has developed. In this mission, the thruster system is required, because of the spin up to deploy the sail using the inertial force, the active notation control and the orbital maneuver to raise the perigee altitude. In the small satellite, the thruster system has to be simple and light weight. In this paper, the gas-liquid equilibrium thruster is developed. This system uses LPG (Liquefied Petroleum Gas) as fuel, so it is easy to handle the system. And this thruster can bring the fuel as liquid in the tank and eject the fuel as gas using the gas liquid equilibrium pressure to produce the thrust, so the fuel tank only needs to resist the vapor pressure of the fuel and the system can be simplified. We show the fundamental performance and the feasibility of this gas-liquid equilibrium thruster. The gas-liquid equilibrium thrusters have the good possibility of the small satellites' thruster system. And if this system would prove its performance in the actual small solar sail mission, this thruster system could be hopeful thruster widely used for the small satellites. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063481021 |