


A four-year BSc in Aerospace Science & Technology at NKUA, covering aerodynamics, propulsion, structures, control, and applied mathematics.
Conservation laws, boundary layers, compressible flow and the aerodynamics of lifting surfaces — the foundation for propulsion, performance and flight analysis.
Operating principles of air-breathing and rocket propulsion — thermodynamic cycles, nozzle flow, thrust and specific impulse, from turbojets to solid motors.
Aircraft equations of motion, static and dynamic stability, and the response of vehicles to control inputs and atmospheric disturbances.
Stress, strain and deformation of aerospace structures — beams, thin-walled sections and an introduction to finite-element methods.
Numerical solution of engineering problems in Python and MATLAB — root-finding, integration, ordinary differential equations and linear systems.

Strong grounding in fluid mechanics, propulsion, flight dynamics, and structural analysis, alongside numerical methods in Python and MATLAB.
Founded ΔV Dynamics, the university's first rocketry team, leading its first solid-motor static fire. View rocketry →
