Low thrust orbit maneuver operations for JAXA geostationary satellites
| العنوان: | Low thrust orbit maneuver operations for JAXA geostationary satellites |
|---|---|
| المؤلفون: | Horii, Michiaki, Dosho, Hirohiko, Mori, Shigehiro, Babauchi, Takao, Uchida, Masashi |
| المصدر: | 宇宙航空研究開発機構特別資料: 低推力・連続加速を用いた宇宙ミッションに関する研究会論文集 = JAXA Special Publication: Collection of Papers Presented at the Meeting on the Study of Space Missions Propelled by Low-Thrust and Sustained Acceleration. :7-12 |
| بيانات النشر: | 宇宙航空研究開発機構, 2008. |
| سنة النشر: | 2008 |
| مصطلحات موضوعية: | Earth observation, ion engine, 軌道制御運用, アークジェットエンジン, electric propulsion, orbit maneuver, 衛星軌道, 低推力推進, イオンエンジン, 地球観測, satellite orbit, arc jet engine, low thrust propulsion, 静止衛星, geostationary satellite, 電気推進, 静止軌道, 比推力, stationary orbit, specific impulse |
| الوصف: | Geostationary satellites need yearly velocity increment of 40 to 50 m/s for the North-Sounth (NS) station keeping. JAXA's recent satellites are adopting low-thrust and high Isp (specific impulse) engines such as DC arc jets and ion engines for the NS station keeping. This paper reports the operation results of such NS maneuvers for the Data Relay Technology Satellite (DRTS: KODAMA) and the Engineering Test Satellite-8 (ETS-8: KIKU No.8). 資料番号: AA0063739002 レポート番号: JAXA-SP-07-020 |
| اللغة: | Japanese |
| تدمد: | 1349-113X |
| URL الوصول: | https://explore.openaire.eu/search/publication?articleId=jairo_______::02792601e182ae78f0ab363ef194bae8 http://id.nii.ac.jp/1696/00005578/ |
| Rights: | OPEN |
| رقم الانضمام: | edsair.jairo.........02792601e182ae78f0ab363ef194bae8 |
| قاعدة البيانات: | OpenAIRE |
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