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EN 1.4958 Stainless Steel vs. EN AC-45300 Aluminum

EN 1.4958 stainless steel belongs to the iron alloys classification, while EN AC-45300 aluminum belongs to the aluminum alloys. There are 29 material properties with values for both materials. Properties with values for just one material (4, 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 1.4958 stainless steel and the bottom bar is EN AC-45300 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
71
Elongation at Break, % 40
1.0 to 2.8
Fatigue Strength, MPa 170
59 to 72
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
27
Tensile Strength: Ultimate (UTS), MPa 630
220 to 290
Tensile Strength: Yield (Proof), MPa 190
150 to 230

Thermal Properties

Latent Heat of Fusion, J/g 300
470
Maximum Temperature: Mechanical, °C 1090
170
Melting Completion (Liquidus), °C 1400
630
Melting Onset (Solidus), °C 1350
590
Specific Heat Capacity, J/kg-K 480
890
Thermal Conductivity, W/m-K 12
150
Thermal Expansion, µm/m-K 15
22

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.7
36
Electrical Conductivity: Equal Weight (Specific), % IACS 2.0
120

Otherwise Unclassified Properties

Base Metal Price, % relative 30
9.5
Density, g/cm3 8.0
2.7
Embodied Carbon, kg CO2/kg material 5.3
8.0
Embodied Energy, MJ/kg 75
150
Embodied Water, L/kg 200
1120

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 190
2.7 to 5.6
Resilience: Unit (Modulus of Resilience), kJ/m3 95
160 to 390
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 24
50
Strength to Weight: Axial, points 22
23 to 29
Strength to Weight: Bending, points 20
30 to 35
Thermal Diffusivity, mm2/s 3.2
60
Thermal Shock Resistance, points 15
10 to 13

Alloy Composition

Aluminum (Al), % 0.2 to 0.5
90.2 to 94.2
Carbon (C), % 0.030 to 0.080
0
Chromium (Cr), % 19 to 22
0
Cobalt (Co), % 0 to 0.5
0
Copper (Cu), % 0 to 0.5
1.0 to 1.5
Iron (Fe), % 41.1 to 50.6
0 to 0.65
Lead (Pb), % 0
0 to 0.15
Magnesium (Mg), % 0
0.35 to 0.65
Manganese (Mn), % 0 to 1.5
0 to 0.55
Nickel (Ni), % 30 to 32.5
0 to 0.25
Niobium (Nb), % 0 to 0.1
0
Nitrogen (N), % 0 to 0.030
0
Phosphorus (P), % 0 to 0.015
0
Silicon (Si), % 0 to 0.7
4.5 to 5.5
Sulfur (S), % 0 to 0.010
0
Tin (Sn), % 0
0 to 0.050
Titanium (Ti), % 0.2 to 0.5
0 to 0.25
Zinc (Zn), % 0
0 to 0.15
Residuals, % 0
0 to 0.15