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S64512 Stainless Steel vs. 5252 Aluminum

S64512 stainless steel belongs to the iron alloys classification, while 5252 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 S64512 stainless steel and the bottom bar is 5252 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 330
68 to 75
Elastic (Young's, Tensile) Modulus, GPa 200
68
Elongation at Break, % 17
4.5 to 11
Fatigue Strength, MPa 540
100 to 110
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
25
Shear Strength, MPa 700
140 to 160
Tensile Strength: Ultimate (UTS), MPa 1140
230 to 290
Tensile Strength: Yield (Proof), MPa 890
170 to 240

Thermal Properties

Latent Heat of Fusion, J/g 270
400
Maximum Temperature: Mechanical, °C 750
180
Melting Completion (Liquidus), °C 1460
650
Melting Onset (Solidus), °C 1420
610
Specific Heat Capacity, J/kg-K 470
910
Thermal Conductivity, W/m-K 28
140
Thermal Expansion, µm/m-K 10
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 3.6
34
Electrical Conductivity: Equal Weight (Specific), % IACS 4.1
120

Otherwise Unclassified Properties

Base Metal Price, % relative 10
9.5
Density, g/cm3 7.8
2.7
Embodied Carbon, kg CO2/kg material 3.3
8.7
Embodied Energy, MJ/kg 47
160
Embodied Water, L/kg 110
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 180
12 to 23
Resilience: Unit (Modulus of Resilience), kJ/m3 2020
210 to 430
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
51
Strength to Weight: Axial, points 40
23 to 30
Strength to Weight: Bending, points 31
31 to 36
Thermal Diffusivity, mm2/s 7.5
57
Thermal Shock Resistance, points 42
10 to 13

Alloy Composition


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Aluminum (Al), % 0
96.6 to 97.8
Carbon (C), % 0.080 to 0.15
0
Chromium (Cr), % 11 to 12.5
0
Copper (Cu), % 0
0 to 0.1
Iron (Fe), % 80.6 to 84.7
0 to 0.1
Magnesium (Mg), % 0
2.2 to 2.8
Manganese (Mn), % 0.5 to 0.9
0 to 0.1
Molybdenum (Mo), % 1.5 to 2.0
0
Nickel (Ni), % 2.0 to 3.0
0
Nitrogen (N), % 0.010 to 0.050
0
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0 to 0.35
0 to 0.080
Sulfur (S), % 0 to 0.025
0
Vanadium (V), % 0.25 to 0.4
0 to 0.050
Zinc (Zn), % 0
0 to 0.050
Residuals, % 0
0 to 0.1