Analisis Kekuatan Uji Tarik dan Bending Filamen Petg (PolyethyleneTerephthalate Glycol) Menggunakan Variasi Suhu dan Variasi Infill Pattern sebagai Material Komponen Landing Skid Drone Dji Mavic 3

Authors

  • Ferdy Ferial Fahmi
  • Denden Mohamad Ariffin

DOI:

https://doi.org/10.54706/senastindo.v7.2025.439

Keywords:

Infill Pattern, PETG Filament, Bending Test, Tensile Test

Abstract

This study investigated the influence of manufacturing parameters—specifically nozzle temperature variations and infill patterns—on the resulting mechanical performance of 3D-printed parts made from PETG filament, tested according to ASTM D638 (tensile) and ASTM D790 (bending) standards. The research successfully identified the tri hexagon infill pattern as superior for load-bearing capability, determined that $240^\circ \text{C}$ was optimal for tensile strength while $230^\circ \text{C}$ was better for bending strength, achieving maximum values of $29.524 \text{ N/mm}^2$ and $13.600 \text{ N/mm}^2$ respectively, ultimately concluding that PETG’s overall strength is less than that of the ABS used in demanding parts like the DJI Mavic 3 Drone components.

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Published

2025-12-28

How to Cite

Ferial Fahmi, F., & Mohamad Ariffin, D. (2025). Analisis Kekuatan Uji Tarik dan Bending Filamen Petg (PolyethyleneTerephthalate Glycol) Menggunakan Variasi Suhu dan Variasi Infill Pattern sebagai Material Komponen Landing Skid Drone Dji Mavic 3. Prosiding Seminar Nasional Sains Teknologi Dan Inovasi Indonesia (SENASTINDO), 7, 159–166. https://doi.org/10.54706/senastindo.v7.2025.439