Environmental Impacts of GTO Objects on LEO
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- HARADA Ryusuke
- Japan Aerospace Exploration Agency
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- KAWAMOTO Satomi
- Japan Aerospace Exploration Agency
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- NAGAOKA Nobuaki
- Japan Aerospace Exploration Agency
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- HANADA Toshiya
- Department of Aeronautics and Astronautics, Kyushu University
説明
<p>The effects of GTO debris to LEO environment are revealed using evolutionary model. GTO debris orbits are modeled as a reference of distribution of actual objects in GTO extracted from JAXA's initial population file. Firstly, three cases of simulation with different perigee altitude were shown taking into accounts the distribution of GTO debris. It indicated that the debris with perigee altitude of over 400 km have long term effects while the debris with perigee altitude of 200 km decay shortly. The effect of continuously generation of GTO debris was secondly investigated. Since the GTO debris has long term orbital life, the number of its debris would keep increasing and accumulate in orbit. Lastly, the risk of GTO debris considering the actual number of debris and future works were discussed. </p>
収録刊行物
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- Journal of Evolving Space Activities
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Journal of Evolving Space Activities 1 (0), n/a-, 2024
宇宙技術および科学の国際シンポジウム
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キーワード
詳細情報 詳細情報について
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- CRID
- 1390862787552867584
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- ISSN
- 27581802
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- 本文言語コード
- en
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- データソース種別
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- JaLC
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- 抄録ライセンスフラグ
- 使用可