The Dynamics sub-team consists of a manager and 4 general members who will be tasked with modeling the trajectory, aerodynamics properties, and stability characteristics of sounding rockets. This will be done with the aid of aerodynamic literature, wind tunnel testing, and analysis tools such as MATLAB and STAR-CCM+. The culmination of this process will be a stable and aerodynamically sound rocket, a product of educated design choices. To accomplish this, members will be expected to consider all factors of a design problem, thoroughly document their work, and be detail-orientated while maintaining a high-level, systems engineering mindset. Members are expected to have an understanding of aerodynamic concepts, and a strong work ethic.