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Influence of Small Satellites' Post-mission Disposal with Enlarging Effective Cross-sectional Area
https://jaxa.repo.nii.ac.jp/records/22448
https://jaxa.repo.nii.ac.jp/records/22448b5b902b6-1f3f-487e-9413-d0bab1009326
Item type | 学術雑誌論文 / Journal Article(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Influence of Small Satellites' Post-mission Disposal with Enlarging Effective Cross-sectional Area | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Space Debris; Small Satellite; Post-mission Disposal | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||
資源タイプ | journal article | |||||
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 |
Ariyoshi, Yuya
× Ariyoshi, Yuya× Hanada, Toshiya× 河本, 聡美× Ariyoshi, Yuya× Hanada, Toshiya× Kawamoto, Satomi |
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著者所属 | ||||||
国立天文台 | ||||||
著者所属 | ||||||
九州大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
National Astronomical Observatory of Japan | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu University | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
出版者 | ||||||
出版者 | 日本航空宇宙学会(JSASS) | |||||
出版者(英) | ||||||
出版者 | The Japan Society for Aeronautical and Space Sciences (JSASS) | |||||
書誌情報 |
en : Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan 巻 12, 号 ists29, p. Pr_21-Pr_25, 発行日 2014-10-30 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Developers of small satellites may think of enlarging their effective cross-sectional area to minimize the long-term presence in the low Earth orbit region. However, the enlargement of their effective cross-sectional area causes the temporal increase of cumulative probability of accidental collisions. This paper evaluates the influence of small satellites’ post-mission disposal by enlarging their cross-sectional area on the future population using an orbital debris environment evolutionary model. According to the result of the future projections, the small satellites’ post-mission disposals by enlarging the effective cross-sectional area have the potential risk of increasing the accidental collision. However small satellites are inserted into orbit below 800 km in this paper, the fragments to be generated by collision expected to decay within short term. The effective number of objects below 2,000 km altitude is not different between the case with post-mission disposals and the case without post-mission disposals. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1884-0485 | |||||
DOI | ||||||
識別子タイプ | DOI | |||||
関連識別子 | http://dx.doi.org/10.2322/tastj.12.Pr_21 | |||||
関連名称 | info:doi/10.2322/tastj.12.Pr_21 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: PA1410089000 |