Missile or Rocket Motion - One Stage with or without Atmospheric Drag

This application calculates the trajectory of the first stage of a LGM-30 Minuteman-III missile when it is launched with an 80 degree inclination to horizonrtal. The calulations can be performed with or without atmospheric drag. The density of air varies with exponentially with

C# (222.2 KB)
 
 
 
 
 
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6/23/2015
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