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Thanks for the answer! I was thinking about an iterative simulation. But I have a problem with that. In order to calculate the drag coeficient I need the Mach number and since I need the Mach number I need the speed of the vehicle and the speed of sound. So, my problem is that I can't determine...

Hi, everybody! I'm looking for a way to calculate the ascent trayectory for a specific rocket. Does somebody know a way to do this? And where can I find the ascent trayectory of the Ariane V? Or any other launcher. Thanks.