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EN 1.4913 Stainless Steel vs. Sintered 6061 Aluminum

EN 1.4913 stainless steel belongs to the iron alloys classification, while sintered 6061 aluminum belongs to the aluminum alloys. There are 29 material properties with values for both materials. Properties with values for just one material (3, 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 1.4913 stainless steel and the bottom bar is sintered 6061 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
68
Elongation at Break, % 14 to 22
0.5 to 6.0
Fatigue Strength, MPa 320 to 480
32 to 62
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 75
25
Tensile Strength: Ultimate (UTS), MPa 870 to 980
83 to 210
Tensile Strength: Yield (Proof), MPa 480 to 850
62 to 190

Thermal Properties

Latent Heat of Fusion, J/g 270
400
Maximum Temperature: Mechanical, °C 700
170
Melting Completion (Liquidus), °C 1460
640
Melting Onset (Solidus), °C 1410
610
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 24
200
Thermal Expansion, µm/m-K 11
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.9
52
Electrical Conductivity: Equal Weight (Specific), % IACS 3.3
170

Otherwise Unclassified Properties

Base Metal Price, % relative 9.0
9.5
Density, g/cm3 7.8
2.7
Embodied Carbon, kg CO2/kg material 2.9
8.3
Embodied Energy, MJ/kg 41
150
Embodied Water, L/kg 97
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 130 to 160
0.68 to 7.0
Resilience: Unit (Modulus of Resilience), kJ/m3 600 to 1860
28 to 280
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
51
Strength to Weight: Axial, points 31 to 35
8.6 to 21
Strength to Weight: Bending, points 26 to 28
16 to 29
Thermal Diffusivity, mm2/s 6.5
81
Thermal Shock Resistance, points 31 to 34
3.8 to 9.4

Alloy Composition

Aluminum (Al), % 0 to 0.020
96 to 99.4
Boron (B), % 0 to 0.0015
0
Carbon (C), % 0.17 to 0.23
0
Chromium (Cr), % 10 to 11.5
0
Copper (Cu), % 0
0 to 0.5
Iron (Fe), % 84.5 to 88.3
0
Magnesium (Mg), % 0
0.4 to 1.2
Manganese (Mn), % 0.4 to 0.9
0
Molybdenum (Mo), % 0.5 to 0.8
0
Nickel (Ni), % 0.2 to 0.6
0
Niobium (Nb), % 0.25 to 0.55
0
Nitrogen (N), % 0.050 to 0.1
0
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0 to 0.5
0.2 to 0.8
Sulfur (S), % 0 to 0.015
0
Vanadium (V), % 0.1 to 0.3
0
Residuals, % 0
0 to 1.5

Comparable Variants