Materials / Compare
DMLS 17-4PH Stainless Steel vs. FDM PAHT-CF
Compare DMLS 17-4PH Stainless Steel vs. FDM PAHT-CF 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 | 861MPasourcemean, as built, horizontal (N=72) | not given (tensile used) |
| Ultimate tensile strength | 886MPasourcemean, as built, horizontal (N=72) | 92MPasourcetypical |
| Flexural strength | not sourced | 125MPasourcetypical |
| Elongation at break | 19.9%sourcemean at break, as built, horizontal | 8.4%sourcetypical |
| Young's modulus (stiffness) | 197GPasourcebase material: wrought 17-4 PH, Condition H 900 (Cleveland-Cliffs) | 3.86GPasourcetypical |
| Density | 7,790kg/m³sourcemean part density (ISO 3369) | 1,060kg/m³sourcetypical |
| Strength to weight | 110kN·m/kg27% higher | 86.8kN·m/kg |
| Stiffness to weight | 25.3MN·m/kg6.94x higher | 3.64MN·m/kg |
| Poisson's ratio | 0.272sourcebase material: wrought 17-4 PH, all conditions (Cleveland-Cliffs) | not sourced |
| Shear modulus | 77.4GPa | not sourced |
| Bulk modulus | 144GPa | not sourced |
| Speed of sound | 5,029m/s | 1,908m/s |
| Thermal | ||
| Thermal conductivity | 17.9W/m·Ksourcebase material: wrought 17-4 PH, Condition H 900, at 149 °C (Cleveland-Cliffs) | not sourced |
| Thermal expansion | 10.4µm/m·Ksourcemean 25-100 °C, ASTM E228, AFTER atmospheric heat treatment (as-built value not published) | not sourced |
| 100 mm part over a 50 °C swing | 52µm growth | not sourced |
| Specific heat | 460J/kg·Ksourcebase material: wrought 17-4 PH, Condition A, 0-100 °C (Cleveland-Cliffs) | not sourced |
| Heats up and cools (diffusivity) | 5mm²/s | not sourced |
| Thermal shock resistance | 5,474W/m | not sourced |
| Melting point | not sourced | 225°Csourcetypical |
| Glass transition | not sourced | 70°Csourcetypical |
| Max service temperature | not sourced | 170°CsourceHDT 1.8 MPa |
| Values for | EOS StainlessSteel 17-4PH IndustryLine (powder 9011-0041), EOS M 290, 40 µm, default job 17-4PH_040_StainlessM291_100, as built, horizontal; ISO 6892 & ASTM E8M | Bambu Lab PAHT-CF, TDS V3.0, printed specimens X-Y, dry state; nozzle 290 °C, bed 100 °C, 100 mm/s, 100% infill; annealed and dried 80 °C for 12 h before testing. |
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 17-4PH Stainless Steel and FDM PAHT-CF are 3D printed: their properties depend on build direction and print settings; these are typical values.
Questions
Is DMLS 17-4PH Stainless Steel stronger than FDM PAHT-CF?
DMLS 17-4PH Stainless Steel is stronger: its yield strength is 861 MPa against tensile strength 92 MPa for FDM PAHT-CF (9.35x).
Which is lighter, DMLS 17-4PH Stainless Steel or FDM PAHT-CF?
FDM PAHT-CF is lighter: 1,060 kg/m³ against 7,790 kg/m³ for DMLS 17-4PH Stainless Steel.
Which is stiffer, DMLS 17-4PH Stainless Steel or FDM PAHT-CF?
DMLS 17-4PH Stainless Steel is stiffer: Young's modulus 197 GPa against 3.86 GPa for FDM PAHT-CF, so the same part in DMLS 17-4PH Stainless Steel deflects less under the same load.
Which is lighter for the same job, DMLS 17-4PH Stainless Steel or FDM PAHT-CF?
For the same stiffness or strength: DMLS 17-4PH Stainless Steel is lighter for a stiff rod or tie (tension), strong rod or tie; FDM PAHT-CF is lighter for a stiff beam (bending), stiff panel or plate, strong beam, strong panel or plate.
| Part that must be | DMLS 17-4PH Stainless Steel | FDM PAHT-CF |
|---|---|---|
| Stiff rod or tie (tension) | lighter | 6.94x heavier |
| Stiff beam (bending) | 3% heavier | lighter |
| Stiff panel or plate | 1.98x heavier | lighter |
| Strong rod or tie | lighter | 27% heavier |
| Strong beam | 1.66x heavier | lighter |
| Strong panel or plate | 2.4x 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).
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