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S41425 Stainless Steel vs. 359.0 Aluminum

S41425 stainless steel belongs to the iron alloys classification, while 359.0 aluminum belongs to the aluminum alloys. There are 31 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 S41425 stainless steel and the bottom bar is 359.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 280
90 to 100
Elastic (Young's, Tensile) Modulus, GPa 200
71
Elongation at Break, % 17
3.8 to 4.9
Fatigue Strength, MPa 450
100
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
27
Shear Strength, MPa 570
220 to 230
Tensile Strength: Ultimate (UTS), MPa 920
340 to 350
Tensile Strength: Yield (Proof), MPa 750
250 to 280

Thermal Properties

Latent Heat of Fusion, J/g 280
530
Maximum Temperature: Mechanical, °C 810
170
Melting Completion (Liquidus), °C 1450
600
Melting Onset (Solidus), °C 1410
570
Specific Heat Capacity, J/kg-K 470
910
Thermal Conductivity, W/m-K 16
140
Thermal Expansion, µm/m-K 10
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.3
35
Electrical Conductivity: Equal Weight (Specific), % IACS 2.7
120

Otherwise Unclassified Properties

Base Metal Price, % relative 13
9.5
Density, g/cm3 7.9
2.6
Embodied Carbon, kg CO2/kg material 2.9
8.0
Embodied Energy, MJ/kg 40
150
Embodied Water, L/kg 120
1090

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 150
12 to 15
Resilience: Unit (Modulus of Resilience), kJ/m3 1420
450 to 540
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 25
54
Strength to Weight: Axial, points 33
37 to 38
Strength to Weight: Bending, points 27
42 to 43
Thermal Diffusivity, mm2/s 4.4
59
Thermal Shock Resistance, points 33
16 to 17

Alloy Composition

Aluminum (Al), % 0
88.9 to 91
Carbon (C), % 0 to 0.050
0
Chromium (Cr), % 12 to 15
0
Copper (Cu), % 0 to 0.3
0 to 0.2
Iron (Fe), % 74 to 81.9
0 to 0.2
Magnesium (Mg), % 0
0.5 to 0.7
Manganese (Mn), % 0.5 to 1.0
0 to 0.1
Molybdenum (Mo), % 1.5 to 2.0
0
Nickel (Ni), % 4.0 to 7.0
0
Nitrogen (N), % 0.060 to 0.12
0
Phosphorus (P), % 0 to 0.020
0
Silicon (Si), % 0 to 0.5
8.5 to 9.5
Sulfur (S), % 0 to 0.0050
0
Titanium (Ti), % 0
0 to 0.2
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15