JAXA Repository / AIREX 未来へ続く、宙(そら)への英知
Other TitleNumerical Analyses of Air Intake for Air Breathing Ion Engine
Author(jpn)小澤, 宇志; 今村, 俊介; 西山, 和孝; 田川, 雅人; 藤田, 和央
Author(eng)Ozawa, Takashi; Imamura, Shunsuke; Nishiyama, Kazutaka; Tagawa, Masahito; Fujita, Kazuhisa
Author Affiliation(jpn)宇宙航空研究開発機構(JAXA); 宇宙航空研究開発機構(JAXA); 宇宙航空研究開発機構(JAXA); 神戸大学; 宇宙航空研究開発機構(JAXA)
Author Affiliation(eng)Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA); Kobe University; Japan Aerospace Exploration Agency (JAXA)
Issue Date2019-02-25
Japan Aerospace Exploration Agency (JAXA)
Publication title宇宙航空研究開発機構特別資料: 第50回流体力学講演会/第36回航空宇宙数値シミュレーション技術シンポジウム論文集
JAXA Special Publication: Proceedings of the 50th Fluid Dynamics Conference / the 36th Aerospace Numerical Simulation Symposium
Start page97
End page101
Publication date2019-02-25
AbstractAt Japan Aerospace Exploration Agency (JAXA), the Super Low Altitude Test Satellite (SLATS), launched in 2017, has been expected to extend space utilization into extremely low earth orbits. Because of the increase of aerodynamic forces acting on the satellite along with the descent of altitude, ion engines have been used for the purpose of maintaining the altitude and attitude of the satellite. To improve the duration of satellites in super low altitude range, the air breathing ion engine (ABIE) has been proposed for future missions. In this work, by carrying out direct simulation Monte Carlo computations, we investigate intake performance for ABIE, especially at 268 km altitude, which is a sun-synchronous recurrent orbit for SLATS.
Description会議情報: 第50回流体力学講演会/第36回航空宇宙数値シミュレーション技術シンポジウム (2018年7月4日-6日. 宮崎市民プラザ), 宮崎市, 宮崎
形態: カラー図版あり
Meeting Information: 50th Fluid Dynamics Conference /the 36th Aerospace Numerical Simulation Symposium (July 4-6, 2018. Miyazaki Citizen's Plaza), Miyazaki, Japan
Physical characteristics: Original contains color illustrations
Document TypeConference Paper
JAXA Category特別資料
NASA Subject CategoryFluid Mechanics and Thermodynamics
Report NoJAXA-SP-18-005

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