Project 33

C4 — Material substitution matrix

Paper claim: Material optimization (quasi-isotropic CFRP, Ti-6Al-4V) yields a 30-40% total mass reduction compared to the baseline 3D printed/aluminum assembly.

Recomputed result: Baseline Mass: 98.1 g Optimized Mass: 62.8 g Mass Reduction: 36.0%

Part Baseline Material Optimized Material Baseline Mass (g) Optimized Mass (g) Delta (g)
Body Tube 7075-T6 CFRP_quasi_iso 42.7 23.6 19.2
Nose Cone PLA PLA 15.5 15.5 0.0
Fin (x4) 7075-T6 CFRP_quasi_iso 38.2 21.1 17.1
Hinge Pin (x4) 7075-T6 Ti-6Al-4V 1.7 2.7 -1.0

Artifact paths:

Deterministic computation — no physical measurement