Aethra
The pilot project
This is the beginning of a process aimed at transforming theoretical knowledge into practical skills. This initial approach is being applied to develop operational solutions for the association's future generations of aircraft.
The first drone built by the association. From design to flight in one academic year.
10 km
Distance covered
15 m/s
Max. velocity
–
Payload capacity
Main material:
Carbon Fibre
Wing Configuration
Mid
Propulsion
Single tractor propeller
Tailplane
conventional
Payload
—
The project began in 2022 and it is based on the SAE Aero Design regulations and culminated in the flight in September 2023.
The wing and tail airfoils are, respectively, SD7062 and NACA 0013.
2.4 m
Length
0.5 m
Height
4.8 m
Wing span
12 kg
Weight
2.15 m2
Wing surface
0.184 m2
Horizontal tail area
2
Flight tests:
Project partners
