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The research project has been made for mathematical modeling of aerospacesystem Space-to-Surface for avoid intercepting process by flight objectsSurface-to-Air. The research has been completed and created mathematical modelswhich used for research and statistical analysis. In mathematical modeling hasbeen including a few models: Model of atmosphere, Model of speed of sound,Model of flight head in space, Model of flight in atmosphere, Models ofnavigation and guidance, Model and statistical analysis of approximation ofaerodynamic characteristics. Modeling has been created for a Space-to-Surfacesystem defined for an optimal trajectory in terminal phase. The modelingincludes models for simulation atmosphere, aerodynamic flight and navigation byan infrared system. The modeling simulation includes statistical analysis ofthe modeling results.

Mathematical Modeling of Aerodynamic Space -to - Surface Flight with Trajectory for Avoid Intercepting Process for Safety and Security Issues