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Prelaunch Estimates of Near Earth Satellite Lifetimes Using Quasi-Dynamic Atmosphere Models - Application to a Proposed Brazilian Satellite

机译:利用准动态大气模型预发射近地卫星寿命估算 - 应用于拟议的巴西卫星

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摘要

A rapid prelaunch estimate of near Earth satellite lifetimes using the small perturbation theory is calculated. A quasi-dynamic atmospheric model is used employing a different exospheric temperature every three months. The drag coefficient is calculated using kinetic theory.

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