Mission params in →
aircraft design out.
A generic mission specification — stall speed, load factor, weight and span limits, endurance objective — goes in as a plain data file. The pipeline searches the design space, evolving the airframe geometry generation by generation against the full constraint set, then lofts the winning design into a buildable outer mold line and characterizes it: drag polar, flight envelope, stability model. No hand geometry at any step.
Everything in the video is real pipeline output — the requirements file, every intermediate geometry in the evolution sequence, the lofted surface, and the performance charts all come from the same recorded run.
The characterized design carries its aerodynamic and stability model with it, so the aircraft can fly in the mission simulation before it exists.