Mass and Stability

Static Margin: 9.9%

CG: 19.28 in

Empty Weight: 23.54 lbs + landing gear

MTOW: 49.53 lbs (Fix)

Payload Mass Fraction: 52% (Fix)

Fuselage

Airfoil: Flat Bottom NACA 4420

Span: 4.906 in

Chord: 12.5 in

Ballast : -12 in, 3.4 lbs %change

Wing

Location: x=26in, z = -4.6 in

Airfoil: MH 200

Span: 30 in

Chord: 6 in

Planform Area: 5 feet^2

Aspect ratio: 5

Aileron

Location:

Span: 12-18in

Chord: 3.6-6in

Canard

Location: x = 0 in, z = 0

Airfoil: MH 201

Span: 65.4 in

Chord: 9.22 in

Vertical Stabilizer

Location: x = 40 in, y = -5 (Flush with fuselage)

Airfoil: NACA 0009

Span: 6.30 in

Chord: 13.5 in