Materials / Compare
Aluminum A380 vs. DMLS Ti-6Al-4V ELI Titanium
Compare Aluminum A380 vs. DMLS Ti-6Al-4V ELI Titanium strength, stiffness, weight and thermal properties.
| Try it on a partA bracket to run stress or thermal on, free in your browser | Open in LessCAD | Open in LessCAD |
|---|---|---|
| Mechanical | ||
| Yield strength | 160MPasourcetypical, 25 °C | 1,100MPasourcetypical, as built, average of horizontal + vertical (M400) |
| Ultimate tensile strength | 320MPasourcetypical, 25 °C | 1,270MPasourcetypical, as built, average of horizontal + vertical (M400) |
| Elongation at break | 3.5%sourcetypical | 8.7%sourcetypical at break, as built (M400) |
| Young's modulus (stiffness) | 71GPasourcetypical, 25 °C | 110GPasourcesame maker and process, sibling grade: EOS Titanium Ti64 (Grade 5) on EOS M 290, as built, XY and Z, typical |
| Density | 2,713kg/m³sourcetypical at 68 °F | 4,400kg/m³sourcetypical part density (ISO 3369), M400 |
| Strength to weight | 59kN·m/kg | 250kN·m/kg4.24x higher |
| Stiffness to weight | 26.2MN·m/kg5% higher | 25MN·m/kg |
| Poisson's ratio | not sourced | 0.342sourcewrought TIMETAL 6-4 (TIMET measurement, mean of 10); composition-level, not DMLS-measured |
| Shear modulus | not sourced | 41GPa |
| Bulk modulus | not sourced | 116GPa |
| Speed of sound | 5,116m/s | 5,000m/s |
| Thermal | ||
| Thermal conductivity | 96.2W/m·Ksourcetypical at 68 °F | 6.6W/m·Ksourcebase material: wrought Ti-6Al-4V / 6-4 ELI (TIMET datasheet), 20 °C |
| Thermal expansion | 21.8µm/m·Ksourcetypical, 68-572 °F (20-300 °C) | 9µm/m·Ksourcemean 25-100 °C, ASTM E228; EOS Ti64 Grade 23 (=ELI) on EOS M 290 40 µm; condition not stated (sheet's mechanical data are heat treated) |
| 100 mm part over a 50 °C swing | 109µm growth | 45µm growth2.42x less |
| Specific heat | 963J/kg·Ksourcetypical at 68 °F | 580J/kg·Ksourcebase material: wrought Ti-6Al-4V / 6-4 ELI (TIMET datasheet), 20 °C |
| Heats up and cools (diffusivity) | 36.8mm²/s14.2x faster | 2.59mm²/s |
| Thermal shock resistance | not sourced | 4,825W/m |
| Melting point | not sourced | 1,630–1,650°Csourcemelting range, wrought TIMETAL 6-4 (composition-level) |
| Values for | A380 aluminium high-pressure die-casting alloy, typical properties; Rheocast Company (aluminium die caster, Germantown WI) A380 alloy data page. | EOS Titanium Ti64ELI (powder 9011-0040; ASTM F136/F3001, i.e. Grade 23) on EOS M400 SF, parameter set Ti64ELI_030_FlexM400_100, 30 µm, as built; ISO 6892-1 A14 |
Every value links to the document that states it. "Not sourced" means no citable source states it (or only a specification minimum); figures computed from it are left out too.
DMLS Ti-6Al-4V ELI Titanium is 3D printed: its properties depend on build direction and print settings; these are typical values.
Questions
Is Aluminum A380 stronger than DMLS Ti-6Al-4V ELI Titanium?
DMLS Ti-6Al-4V ELI Titanium is stronger: its yield strength is 1,100 MPa against 160 MPa for Aluminum A380 (6.88x).
Which is lighter, Aluminum A380 or DMLS Ti-6Al-4V ELI Titanium?
Aluminum A380 is lighter: 2,713 kg/m³ against 4,400 kg/m³ for DMLS Ti-6Al-4V ELI Titanium.
Which is stiffer, Aluminum A380 or DMLS Ti-6Al-4V ELI Titanium?
DMLS Ti-6Al-4V ELI Titanium is stiffer: Young's modulus 110 GPa against 71 GPa for Aluminum A380, so the same part in DMLS Ti-6Al-4V ELI Titanium deflects less under the same load.
Which is lighter for the same job, Aluminum A380 or DMLS Ti-6Al-4V ELI Titanium?
For the same stiffness or strength: Aluminum A380 is lighter for a stiff rod or tie (tension), stiff beam (bending), stiff panel or plate; DMLS Ti-6Al-4V ELI Titanium is lighter for a strong rod or tie, strong beam, strong panel or plate.
| Part that must be | Aluminum A380 | DMLS Ti-6Al-4V ELI Titanium |
|---|---|---|
| Stiff rod or tie (tension) | lighter | 5% heavier |
| Stiff beam (bending) | lighter | 30% heavier |
| Stiff panel or plate | lighter | 40% heavier |
| Strong rod or tie | 4.24x heavier | lighter |
| Strong beam | 2.23x heavier | lighter |
| Strong panel or plate | 1.62x heavier | lighter |
For the same stiffness or strength, mass scales with density over stiffness (or strength) raised to a power set by how the part is loaded: 1 for a rod in tension, 1/2 for a beam in bending, 1/3 for a panel (the standard material-selection indices).
Which conducts heat better, Aluminum A380 or DMLS Ti-6Al-4V ELI Titanium?
Aluminum A380 conducts heat better: 96.2 W/m·K against 6.6 W/m·K for DMLS Ti-6Al-4V ELI Titanium.
Which expands less with temperature?
DMLS Ti-6Al-4V ELI Titanium expands less: 9 µm/m·K against 21.8 µm/m·K for Aluminum A380.
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