Table 3

Main features of the concept “J170” of flat-upper-surface-joined-wing UAV

PlanformSwept airfoils
in a rhombus
arrangement
Wing span3 m
MAC0.17 m
Reference area1.02 m2
Aspect ratio17.6
Taper ratio1
Vertical distance between front and back airfoil0.25 m
Dihedral6 deg
Number of solar cells48
MTOW3.5 kg
Estimated time to altitude 10 km4 h
Maximum airspeed12–17 m/s
Source: Table by authors

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