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S40975 Stainless Steel vs. A360.0 Aluminum

S40975 stainless steel belongs to the iron alloys classification, while A360.0 aluminum belongs to the aluminum alloys. There are 31 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 S40975 stainless steel and the bottom bar is A360.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 170
75
Elastic (Young's, Tensile) Modulus, GPa 190
72
Elongation at Break, % 22
1.6 to 5.0
Fatigue Strength, MPa 210
82 to 150
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 75
27
Shear Strength, MPa 290
180
Tensile Strength: Ultimate (UTS), MPa 460
180 to 320
Tensile Strength: Yield (Proof), MPa 310
170 to 260

Thermal Properties

Latent Heat of Fusion, J/g 270
530
Maximum Temperature: Mechanical, °C 710
170
Melting Completion (Liquidus), °C 1450
680
Melting Onset (Solidus), °C 1400
590
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 26
110
Thermal Expansion, µm/m-K 10
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.9
30
Electrical Conductivity: Equal Weight (Specific), % IACS 3.3
100

Otherwise Unclassified Properties

Base Metal Price, % relative 6.5
9.5
Density, g/cm3 7.8
2.6
Embodied Carbon, kg CO2/kg material 2.0
7.8
Embodied Energy, MJ/kg 28
150
Embodied Water, L/kg 95
1070

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 93
4.6 to 13
Resilience: Unit (Modulus of Resilience), kJ/m3 250
190 to 470
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 25
53
Strength to Weight: Axial, points 17
19 to 34
Strength to Weight: Bending, points 17
27 to 39
Thermal Diffusivity, mm2/s 7.0
48
Thermal Shock Resistance, points 17
8.5 to 15

Alloy Composition

Aluminum (Al), % 0
85.8 to 90.6
Carbon (C), % 0 to 0.030
0
Chromium (Cr), % 10.5 to 11.7
0
Copper (Cu), % 0
0 to 0.6
Iron (Fe), % 84.4 to 89
0 to 1.3
Magnesium (Mg), % 0
0.4 to 0.6
Manganese (Mn), % 0 to 1.0
0 to 0.35
Nickel (Ni), % 0.5 to 1.0
0 to 0.5
Nitrogen (N), % 0 to 0.030
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0 to 1.0
9.0 to 10
Sulfur (S), % 0 to 0.030
0
Tin (Sn), % 0
0 to 0.15
Titanium (Ti), % 0 to 0.75
0
Zinc (Zn), % 0
0 to 0.5
Residuals, % 0
0 to 0.25