CAD/Slicer Data:

• Wall thickness: .125
• Length: 5
• Diameter: 6
• Volume: 14.40 in^3
• Surface Area: 117.5in^2
• Predicted mass: 55.03g [.121 lbs]

Slicer Settings:

• 0.24mm Draft BBL X1C
• Concentric top/bottom shells
  • 4 top/bottom shell layers
• 15% sparse infill density
  • Adaptive cubic infill

Section Weight Estimation:

• Fuselage Section Weight Estimation Method

$$ \boxed{W_{fusesec,approx}=[W_{ASA}+1.5*(4*A_{surf,fusesec}*W_{glass/area})]} $$

• $W_{ASA}=.121lbs$
• $A_{surf,fusesec}=118in^2$
• $W_{glass/area}=2.74oz/yd^2=1.32*10^{-4}lbs/in^2$

$$ W_{fusesec,approx}=0.121+1.5*[4118(1.32*10^{-4})]=0.2145lbs\\W_{fusesec,approx} \approx 0.22lbs $$