EN 1.4378 Stainless Steel vs. Sintered 2014 Aluminum
EN 1.4378 stainless steel belongs to the iron alloys classification, while sintered 2014 aluminum belongs to the aluminum alloys. There are 25 material properties with values for both materials. Properties with values for just one material (8, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.
For each property being compared, the top bar is EN 1.4378 stainless steel and the bottom bar is sintered 2014 aluminum.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 200 | |
70 |
Elongation at Break, % | 14 to 34 | |
0.5 to 3.0 |
Fatigue Strength, MPa | 340 to 550 | |
52 to 100 |
Poisson's Ratio | 0.28 | |
0.33 |
Shear Modulus, GPa | 77 | |
26 |
Tensile Strength: Ultimate (UTS), MPa | 760 to 1130 | |
140 to 290 |
Tensile Strength: Yield (Proof), MPa | 430 to 970 | |
97 to 280 |
Thermal Properties
Latent Heat of Fusion, J/g | 290 | |
390 |
Maximum Temperature: Mechanical, °C | 910 | |
170 |
Melting Completion (Liquidus), °C | 1390 | |
650 |
Melting Onset (Solidus), °C | 1350 | |
560 |
Specific Heat Capacity, J/kg-K | 480 | |
880 |
Thermal Expansion, µm/m-K | 17 | |
23 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 12 | |
10 |
Density, g/cm3 | 7.6 | |
2.9 |
Embodied Carbon, kg CO2/kg material | 2.7 | |
8.0 |
Embodied Energy, MJ/kg | 39 | |
150 |
Embodied Water, L/kg | 150 | |
1150 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 150 to 220 | |
1.0 to 5.7 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 470 to 2370 | |
68 to 560 |
Stiffness to Weight: Axial, points | 14 | |
13 |
Stiffness to Weight: Bending, points | 25 | |
47 |
Strength to Weight: Axial, points | 28 to 41 | |
13 to 27 |
Strength to Weight: Bending, points | 24 to 31 | |
20 to 33 |
Thermal Shock Resistance, points | 16 to 23 | |
6.2 to 13 |
Alloy Composition
Aluminum (Al), % | 0 | |
91.5 to 96.3 |
Carbon (C), % | 0 to 0.080 | |
0 |
Chromium (Cr), % | 17 to 19 | |
0 |
Copper (Cu), % | 0 | |
3.5 to 5.0 |
Iron (Fe), % | 61.2 to 69 | |
0 |
Magnesium (Mg), % | 0 | |
0.2 to 0.8 |
Manganese (Mn), % | 11.5 to 14.5 | |
0 |
Nickel (Ni), % | 2.3 to 3.7 | |
0 |
Nitrogen (N), % | 0.2 to 0.4 | |
0 |
Phosphorus (P), % | 0 to 0.060 | |
0 |
Silicon (Si), % | 0 to 1.0 | |
0 to 1.2 |
Sulfur (S), % | 0 to 0.030 | |
0 |
Residuals, % | 0 | |
0 to 1.5 |