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Estimating the lifetime and Reentry of the Aluminum Space Debris of Sizes (1-10 cm) in LEO under Atmosphere Drag Effects

  This study concerns in addressing the lifetime and reentry of the space debris in LEO which extends from 200 to 1200 km. In this study the new Computer programs are designed to simulate orbit dynamics of space debris lifetime and reentry under atmospheric drag force by using Runge-Kutta Method t...

詳細記述

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書誌詳細
主要な著者: H. K. Al-Zaidi, A.M. Taleb, M. J. Al-Bermani
フォーマット: Artigo
言語:Inglês
出版事項: University of Kufa 2020-12-01
シリーズ:Journal of Kufa-Physics
主題:
オンライン・アクセス:https://journal.uokufa.edu.iq/index.php/jkp/article/view/7439
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