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S15700 Stainless Steel vs. 332.0 Aluminum

S15700 stainless steel belongs to the iron alloys classification, while 332.0 aluminum belongs to the aluminum alloys. There are 31 material properties with values for both materials. Properties with values for just one material (2, 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 S15700 stainless steel and the bottom bar is 332.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 200 to 460
110
Elastic (Young's, Tensile) Modulus, GPa 200
73
Elongation at Break, % 1.1 to 29
1.0
Fatigue Strength, MPa 370 to 770
90
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
27
Shear Strength, MPa 770 to 1070
190
Tensile Strength: Ultimate (UTS), MPa 1180 to 1890
250
Tensile Strength: Yield (Proof), MPa 500 to 1770
190

Thermal Properties

Latent Heat of Fusion, J/g 290
530
Maximum Temperature: Mechanical, °C 870
170
Melting Completion (Liquidus), °C 1440
580
Melting Onset (Solidus), °C 1400
530
Specific Heat Capacity, J/kg-K 480
880
Thermal Conductivity, W/m-K 16
100
Thermal Expansion, µm/m-K 11
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.3
26
Electrical Conductivity: Equal Weight (Specific), % IACS 2.6
84

Otherwise Unclassified Properties

Base Metal Price, % relative 15
10
Density, g/cm3 7.8
2.8
Embodied Carbon, kg CO2/kg material 3.4
7.8
Embodied Energy, MJ/kg 47
140
Embodied Water, L/kg 140
1040

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 17 to 270
2.3
Resilience: Unit (Modulus of Resilience), kJ/m3 640 to 4660
250
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 42 to 67
24
Strength to Weight: Bending, points 32 to 43
31
Thermal Diffusivity, mm2/s 4.2
42
Thermal Shock Resistance, points 39 to 63
12

Alloy Composition


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Aluminum (Al), % 0.75 to 1.5
80.1 to 89
Carbon (C), % 0 to 0.090
0
Chromium (Cr), % 14 to 16
0
Copper (Cu), % 0
2.0 to 4.0
Iron (Fe), % 69.6 to 76.8
0 to 1.2
Magnesium (Mg), % 0
0.5 to 1.5
Manganese (Mn), % 0 to 1.0
0 to 0.5
Molybdenum (Mo), % 2.0 to 3.0
0
Nickel (Ni), % 6.5 to 7.7
0 to 0.5
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0 to 1.0
8.5 to 10.5
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0 to 0.25
Zinc (Zn), % 0
0 to 1.0
Residuals, % 0
0 to 0.5