The Mission Analysis team is responsible for the preliminary design and aerodynamic optimization of the rocket with proprietary and commercial tools such as ANSYS Fluent, as well as the study of the trajectory with ASTOS from the design phase to launch day. Both static and dynamic stability analysis are also carried out with customized aerodynamic models and Montecarlo simulations to study the flight under different launch conditions and use it to estimate the apogee and landing points. In addition, it is responsible for the development of internal software for the design, optimization and flight simulation of rockets with aerodynamic and dynamic models with 6 degrees of freedom.