| Item type |
会議発表論文 / Conference Paper(1) |
| 公開日 |
2015-07-07 |
| タイトル |
|
|
タイトル |
Structure design of the telescope for Small-JASMINE program |
|
言語 |
en |
| 言語 |
|
|
言語 |
eng |
| 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 |
| 著者 |
Utsunomiya, Shin
Yasuda, Susumu
Yano, Taihei
Niwa, Yoshito
Kobayashi, Yukiyasu
Kashima, Shingo
Goda, Naoteru
Yamada, Yoshiyuki
|
| 著者所属（英） |
|
|
|
en |
|
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Japan Aerospace Exploration Agency(JAXA) |
| 著者所属（英） |
|
|
|
en |
|
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Japan Aerospace Exploration Agency(JAXA) |
| 著者所属（英） |
|
|
|
en |
|
|
National Astronomical Observatory of Japan(NAOJ) |
| 著者所属（英） |
|
|
|
en |
|
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National Astronomical Observatory of Japan(NAOJ) |
| 著者所属（英） |
|
|
|
en |
|
|
National Astronomical Observatory of Japan(NAOJ) |
| 著者所属（英） |
|
|
|
en |
|
|
National Astronomical Observatory of Japan(NAOJ) |
| 著者所属（英） |
|
|
|
en |
|
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National Astronomical Observatory of Japan(NAOJ) |
| 著者所属（英） |
|
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|
en |
|
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Kyoto University |
| 出版者 |
|
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出版者 |
国際光工学会(SPIE) |
| 出版者（英） |
|
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出版者 |
The International Society for Optical Engineering(SPIE) |
| 書誌情報 |
en : Proceedings of SPIE
巻 9143,
発行日 2014-08-02
|
| 会議概要（会議名, 開催地, 会期, 主催者等）（英） |
|
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内容記述タイプ |
Other |
|
内容記述 |
SPIE 9143, Space Telescopes and Instrumentation 2014: Optical, Infrared, and Millimeter Wave, 91430Z(June 22-27, 2014. Palais des congrès de Montréal), Montréal, Quebec, Canada. |
| 抄録（英） |
|
|
内容記述タイプ |
Other |
|
内容記述 |
Small-JASMINE program (Japan Astrometry Satellite Mission for INfrared Exploration) is one of applicants for JAXA (Japan Aerospace Exploration Agency) space science missions launched by Epsilon Launch Vehicles, and now being reviewed in the Science Committee of ISAS (Institute of Space and Astronautical Science), JAXA. Telescope of 300 mm aperture diameter will focus to the central region of the Milky Way Galactic. The target of Small-JASMINE is to obtain reliable measurements of extremely small stellar motions with the highest accuracy of 10 μ arcseconds and to provide precise distances and velocities of multitudes of stars up to 30,000 light years. Preliminary Structure design of Small- JASMINE has been done and indicates to satisfy all of requirements from the mission requirement, the system requirement, Epsilon Launch conditions and interfaces of the small science satellite standard bus. High margin of weight for the mission allows using all super invar structure that may reduce unforeseen thermal distortion risk especially caused by connection of different materials. Thermal stability of the telescope is a key issue and should be verified in a real model at early stage of the development. |
| ISSN |
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|
収録物識別子タイプ |
ISSN |
|
収録物識別子 |
0277-786X |
| DOI |
|
|
|
識別子タイプ |
DOI |
|
|
関連識別子 |
http://dx.doi.org/10.1117/12.2055929 |
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|
関連名称 |
info:doi/10.1117/12.2055929 |
| 資料番号 |
|
|
内容記述タイプ |
Other |
|
内容記述 |
資料番号: PA1510036000 |
