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The present project will simulate a space launch vehicle trajectory for given launcher and external conditions. It also will give an optimal solution for this trajectory when trajectory parameters are not fixed.
Simulación, Astronáutica, Lanzadera espacial, Ingeniería aeroespacial, Aeronáutica
Simulación, Astronáutica, Lanzadera espacial, Ingeniería aeroespacial, Aeronáutica
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