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Instability of the Current Space Debris Population in Low Earth Orbit
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- MANIWA Kazuaki
- 九州大学大学院工学府航空宇宙工学専攻
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- HANADA Toshiya
- 九州大学大学院工学研究院航空宇宙工学部門
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- KAWAMOTO Satomi
- 宇宙航空研究開発機構研究開発本部
Bibliographic Information
- Other Title
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- 地球低軌道における軌道環境の安定性について
- チキュウ テイキドウ ニ オケル キドウ カンキョウ ノ アンテイセイ ニ ツイテ
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Description
Since the launch of Sputnik, orbital debris population continues to increase due to ongoing space activities, on-orbit explosions, and accidental collisions. In the future, it is expected that a great deal of fragments will be created by explosions and collisions. Thus, the number of space debris may increase exponentially (Kessler Syndrome). This paper analyzes the Kessler Syndrome using the Low Earth Orbital Debris Environmental Evolutionary Model (LEODEEM) developed at Kyushu University with collaboration from JAXA. The purpose of the study aims at understanding the issues related to space environment conservation. The results provide effective conditions of Active Debris Removal which is one of the space debris mitigation procedures.
Journal
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- JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 58 (674), 83-89, 2010
THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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Details 詳細情報について
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- CRID
- 1390282679445767168
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- NII Article ID
- 10026520679
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- NII Book ID
- AA11307372
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- ISSN
- 24323691
- 13446460
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- NDL BIB ID
- 10619476
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- Text Lang
- ja
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- Data Source
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- JaLC
- NDL Search
- Crossref
- CiNii Articles
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- Abstract License Flag
- Disallowed