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A Microscale Solar Sail
https://jaxa.repo.nii.ac.jp/records/7375
https://jaxa.repo.nii.ac.jp/records/73753d447af4-044d-4dc8-89e9-5eb28e6b613e
| Item type | 会議発表論文 / Conference Paper(1) | |||||||||
|---|---|---|---|---|---|---|---|---|---|---|
| 公開日 | 2015-03-26 | |||||||||
| タイトル | ||||||||||
| タイトル | A Microscale Solar Sail | |||||||||
| 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 |
Atchison, Justin A.
× Atchison, Justin A.
× Peck, Mason A.
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| 著者所属（英） | ||||||||||
| en | ||||||||||
| Sibley School of Mechanical and Aerospace Engineering, Cornell University | ||||||||||
| 著者所属（英） | ||||||||||
| en | ||||||||||
| Sibley School of Mechanical and Aerospace Engineering, Cornell University | ||||||||||
| 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) | |||||||||
| 書誌情報 |
アストロダイナミクスシンポジウム講演後刷り集 en : Proceedings of 18th workshop on JAXA Astrodynamics and flight mechanics 巻 2008, p. 1-14, 発行日 2009-03 |
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| 会議概要（会議名, 開催地, 会期, 主催者等）（英） | ||||||||||
| 内容記述タイプ | Other | |||||||||
| 内容記述 | Symposium on Flight Mechanics and Astrodynamics 2008 (July 28-29, 2008. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)), Sagamihara, Kanagawa Japan | |||||||||
| 抄録（英） | ||||||||||
| 内容記述タイプ | Other | |||||||||
| 内容記述 | We consider spacecraft length scaling as a means of enabling achieving passive, feasible infinite-impulse orbits. Taking inspiration from the orbital dynamics of dust, this paper discusses the consequences of length scaling on acceleration due to solar radiation pressure and demonstrates its effectiveness on a candidate microscale spacecraft. We propose to fabricate this dime-sized spacecraft on a single ultra-thin substrate of silicon. This choice reduces the total mass to fewer than 7.5 mg and makes the spacecraft bus itself a solar sail, yielding a lightness number beta of 0.0175. This architecture can provide passive solar sail formations and various passive methods of changing orbital energy. The paper surveys and compares passive methods of achieving a marginally stable sun-pointing attitude including the addition of fixed vanes and optical grating of the surface. The microscale infinite impulse (MII) spacecraft design replaces the traditional spacecraft subsystems with a single integrated circuit (IC). Our current fabrication efforts are directed at realizing this spacecraft as a simple sensing and transmitting circuit with standard IC methods. | |||||||||
| 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 | |||||||||
| 書誌レコードID | ||||||||||
| 収録物識別子タイプ | NCID | |||||||||
| 収録物識別子 | AA11567475 | |||||||||
| 資料番号 | ||||||||||
| 内容記述タイプ | Other | |||||||||
| 内容記述 | 資料番号: AA0064733001 | |||||||||
