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This is an attempt to develop a code to obtain the reentry trajectory of a space vehicle which a certain velocity, altitude and rentry angle. There are many thing that can be included to make this more sophisticated and changes to obtain more accurate and real life results.
Project done while doing internship at SSERD, India under the guidance of Gautham Barathwaj.
Reentry-Trajectory
American Standard Model of Atmospheric Temperature is used for modelling density.
First order scheme explicit numerical method used to solution.
About
This is an attempt to develop a code to obtain the reentry trajectory of a space vehicle which a certain velocity, altitude and rentry angle. There are many thing that can be included to make this more sophisticated and changes to obtain more accurate and real life results.