
High-speed STOL UAV
I led the mechanical design of a carbon-fibre UAV built for short takeoff and landing, taking it from SolidWorks models and structural and aerodynamic analysis to fabricated, assembled hardware.
- Lighter airframe, with required safety factors heldDesign result from analysis
- 12%
- SolidWorks parts, assemblies and GD&T fabrication drawings
- 40+

Fuselage modelled as a thin shell with internal bulkheads in SolidWorks. 
Team assembly on the bench, with the tail boom and a tail surface laid out. 
Inside the fuselage — servos, wiring and power distribution.





