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