Materials / Compare
DMLS AlSi10Mg Aluminum vs. DMLS Ti-6Al-4V ELI Titanium
Compare DMLS AlSi10Mg Aluminum vs. DMLS Ti-6Al-4V ELI Titanium strength, stiffness, weight and thermal properties.
| Mechanical | DMLS AlSi10Mg Aluminum | DMLS Ti-6Al-4V ELI Titanium |
|---|---|---|
| Yield strength | 270MPa1 | 1,100MPa24.07x stronger |
| Ultimate tensile strength | 450MPa1 | 1,270MPa22.82x stronger |
| Elongation at break | 10.2%117% more ductile | 8.7%2 |
| Young's modulus (stiffness) | 72GPa3 | same maker and process110GPa41.53x stiffer |
| Density | 2,670kg/m³51.65x lighter | 4,400kg/m³2 |
| Strength to weight | 101kN·m/kg | 250kN·m/kg2.47x higher |
| Stiffness to weight | 27MN·m/kg8% higher | 25MN·m/kg |
| Poisson's ratio | base material0.336 | wrought TIMETAL 6-40.3427 |
| Shear modulus | 27.1GPa | 41GPa1.51x stiffer in shear |
| Bulk modulus | 70.6GPa | 116GPa1.64x higher |
| Speed of sound | 5,193m/s4% faster | 5,000m/s |
| Thermal | DMLS AlSi10Mg Aluminum | DMLS Ti-6Al-4V ELI Titanium |
|---|---|---|
| Thermal conductivity | 110W/m·K116.7x more heat through a fin | base material6.6W/m·K8 |
| Thermal expansion | mean 25-100 °C20µm/m·K1 | mean 25-100 °C9µm/m·K92.22x less |
| 100 mm part over a 50 °C swing | 100µm growth | 45µm growth2.22x less |
| Specific heat | base material963J/kg·K6 | base material580J/kg·K8 |
| Heats up and cools (diffusivity) | 42.8mm²/s16.5x faster | 2.59mm²/s |
| Thermal shock resistance | 13,819W/m2.86x more resistant | 4,825W/m |
| Melting point | not sourced | melting range1,630–1,650°C7 |
| Try it on a partA bracket to run stress or thermal on, free in your browser | Open in LessCAD | Open in LessCAD |
|---|
Sources9 documents: EOS GmbH, Renishaw, U.S. Department of Defense, TIMET
- DMLS AlSi10Mg Aluminum
- EOS Aluminium AlSi10Mg (powder 9011-0024), EOS M 290 | 30 µm process (AlSi10Mg_FlexM291 2.01), as manufactured, horizontal; machined (turned) specimens, ISO 6892-1 B10
- DMLS Ti-6Al-4V ELI Titanium
- 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
- 1EOS Aluminium AlSi10Mg Material Data SheetEOS GmbHarchived copyDMLS AlSi10Mg Aluminum · Yield strength: typical, as manufactured, horizontalDMLS AlSi10Mg Aluminum · Ultimate tensile strength: typical, as manufactured, horizontalDMLS AlSi10Mg Aluminum · Elongation at break: typical at break, as manufactured, horizontalDMLS AlSi10Mg Aluminum · Thermal conductivity: typical, as manufactured, horizontal (ISO 22007-2)DMLS AlSi10Mg Aluminum · Thermal expansion: mean 25-100 °C, ASTM E228
- 2EOS Titanium Ti64ELI Material Data Sheet, M 290 and M 400EOS GmbHarchived copyDMLS Ti-6Al-4V ELI Titanium · Yield strength: typical, as built, average of horizontal + vertical (M400)DMLS Ti-6Al-4V ELI Titanium · Ultimate tensile strength: typical, as built, average of horizontal + vertical (M400)DMLS Ti-6Al-4V ELI Titanium · Elongation at break: typical at break, as built (M400)DMLS Ti-6Al-4V ELI Titanium · Density: typical part density (ISO 3369), M400
- 3RenAM 500 Series Aluminium AlSi10Mg Material Data SheetRenishawDMLS AlSi10Mg Aluminum · Young's modulus (stiffness): same material and process, different machine maker: Renishaw RenAM 500, 30 µm, as built, horizontal (XY)
- 4EOS Titanium Ti64 Material Data Sheet, M 290 (2022)EOS GmbHarchived copyDMLS Ti-6Al-4V ELI Titanium · Young's modulus (stiffness): same maker and process, sibling grade: EOS Titanium Ti64 (Grade 5) on EOS M 290, as built, XY and Z, typical
- 5EOS Aluminium AlSi10Mg Material Data Sheet, FlexLine, M 290 (2018)EOS GmbHarchived copyDMLS AlSi10Mg Aluminum · Density: typical part density (ISO 3369), EOS M 290, AlSi10Mg_030_FlexM291 (30 µm)
- 6MIL-HDBK-5J, Metallic Materials and Elements for Aerospace Vehicle Structures (2003)U.S. Department of DefenseDMLS AlSi10Mg Aluminum · Poisson's ratio: base material: cast Al-Si-Mg alloy 359.0 (Al-9Si-0.6Mg, closest MIL-HDBK-5J alloy to AlSi10Mg / EN AC-43000)DMLS AlSi10Mg Aluminum · Specific heat: base material: cast Al-Si-Mg alloy 359.0 (MIL-HDBK-5J), at 100 °C
- 7TIMETAL 6-4 PropertiesTIMETarchived copyDMLS Ti-6Al-4V ELI Titanium · Poisson's ratio: wrought TIMETAL 6-4 (TIMET measurement, mean of 10); composition-level, not DMLS-measuredDMLS Ti-6Al-4V ELI Titanium · Melting point: melting range, wrought TIMETAL 6-4 (composition-level)
- 8TIMETAL 6-4 Data SheetTIMETarchived copyDMLS Ti-6Al-4V ELI Titanium · Thermal conductivity: base material: wrought Ti-6Al-4V / 6-4 ELI (TIMET datasheet), 20 °CDMLS Ti-6Al-4V ELI Titanium · Specific heat: base material: wrought Ti-6Al-4V / 6-4 ELI (TIMET datasheet), 20 °C
- 9EOS Titanium Ti64 Grade 23 Material Data SheetEOS GmbHarchived copyDMLS Ti-6Al-4V ELI Titanium · Thermal expansion: mean 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)
Each number points to the document that states it, with the exact basis. Values without a number are computed from the sourced ones. "Not sourced" means no citable source states it (or only a specification minimum); figures computed from it are left out too.
DMLS AlSi10Mg Aluminum and DMLS Ti-6Al-4V ELI Titanium are 3D printed: their properties depend on build direction and print settings; these are typical values.
Questions
Mechanical
Is DMLS AlSi10Mg Aluminum stronger than DMLS Ti-6Al-4V ELI Titanium?
DMLS Ti-6Al-4V ELI Titanium is stronger: its yield strength is 1,100 MPa against 270 MPa for DMLS AlSi10Mg Aluminum (4.07x).
Which is lighter, DMLS AlSi10Mg Aluminum or DMLS Ti-6Al-4V ELI Titanium?
DMLS AlSi10Mg Aluminum is lighter: 2,670 kg/m³ against 4,400 kg/m³ for DMLS Ti-6Al-4V ELI Titanium.
Which is stiffer, DMLS AlSi10Mg Aluminum or DMLS Ti-6Al-4V ELI Titanium?
DMLS Ti-6Al-4V ELI Titanium is stiffer: Young's modulus 110 GPa against 72 GPa for DMLS AlSi10Mg Aluminum, so the same part in DMLS Ti-6Al-4V ELI Titanium deflects less under the same load.
Which is lighter for the same job, DMLS AlSi10Mg Aluminum or DMLS Ti-6Al-4V ELI Titanium?
For the same stiffness or strength: DMLS AlSi10Mg Aluminum 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 | DMLS AlSi10Mg Aluminum | DMLS Ti-6Al-4V ELI Titanium |
|---|---|---|
| Stiff rod or tie (tension) | lighter | 8% heavier |
| Stiff beam (bending) | lighter | 33% heavier |
| Stiff panel or plate | lighter | 43% heavier |
| Strong rod or tie | 2.47x heavier | lighter |
| Strong beam | 1.55x heavier | lighter |
| Strong panel or plate | 22% 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 is more ductile, DMLS AlSi10Mg Aluminum or DMLS Ti-6Al-4V ELI Titanium?
DMLS AlSi10Mg Aluminum stretches further before it breaks: 10.2% elongation at break against 8.7% for DMLS Ti-6Al-4V ELI Titanium.
Thermal
Which conducts heat better, DMLS AlSi10Mg Aluminum or DMLS Ti-6Al-4V ELI Titanium?
DMLS AlSi10Mg Aluminum conducts heat better: 110 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 20 µm/m·K for DMLS AlSi10Mg Aluminum.
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