Span

b = 39

Wing Area

S = 155 ft²

Aspect Ratio

AR = 9.81

Wing Chord

c = 4 ft

Airfoil

NACA 8-H-12

L.E. Sweep

13^o

Weight Empty

W_e = 370 lb

Flight Weight (max)

W = 573 lb

Wing Loading

W/S = 3.68 lb/ft²

Max. Glide Ratio

L/D_max = 28
@ V_c = 51 mph

Min. Sink Rate

w_min = 150 ft/min
@ V_c = 43 mph

Stall Speed

V_c = 43 mph

Max. Lift Coefficient

C_Lmax = 1.24

Min Drag Coefficient

C_Dmin = 0.0125