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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...

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Hlavní autoři: H. K. Al-Zaidi, A.M. Taleb, M. J. Al-Bermani
Médium: Artigo
Jazyk:Inglês
Vydáno: University of Kufa 2020-12-01
Edice:Journal of Kufa-Physics
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On-line přístup:https://journal.uokufa.edu.iq/index.php/jkp/article/view/7439
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