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S20161 Stainless Steel vs. 1050A Aluminum

S20161 stainless steel belongs to the iron alloys classification, while 1050A 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 S20161 stainless steel and the bottom bar is 1050A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 250
20 to 45
Elastic (Young's, Tensile) Modulus, GPa 190
68
Elongation at Break, % 46
1.1 to 33
Fatigue Strength, MPa 360
22 to 55
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
26
Shear Strength, MPa 690
44 to 97
Tensile Strength: Ultimate (UTS), MPa 980
68 to 170
Tensile Strength: Yield (Proof), MPa 390
22 to 150

Thermal Properties

Latent Heat of Fusion, J/g 330
400
Maximum Temperature: Mechanical, °C 870
170
Melting Completion (Liquidus), °C 1380
660
Melting Onset (Solidus), °C 1330
650
Specific Heat Capacity, J/kg-K 490
900
Thermal Conductivity, W/m-K 15
230
Thermal Expansion, µm/m-K 16
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.5
59
Electrical Conductivity: Equal Weight (Specific), % IACS 2.9
200

Otherwise Unclassified Properties

Base Metal Price, % relative 12
9.0
Density, g/cm3 7.5
2.7
Embodied Carbon, kg CO2/kg material 2.7
8.2
Embodied Energy, MJ/kg 39
150
Embodied Water, L/kg 130
1200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 360
1.9 to 19
Resilience: Unit (Modulus of Resilience), kJ/m3 390
3.7 to 160
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 26
50
Strength to Weight: Axial, points 36
6.9 to 18
Strength to Weight: Bending, points 29
14 to 25
Thermal Diffusivity, mm2/s 4.0
94
Thermal Shock Resistance, points 22
3.0 to 7.6

Alloy Composition

Aluminum (Al), % 0
99.5 to 100
Carbon (C), % 0 to 0.15
0
Chromium (Cr), % 15 to 18
0
Copper (Cu), % 0
0 to 0.050
Iron (Fe), % 65.6 to 73.9
0 to 0.4
Magnesium (Mg), % 0
0 to 0.050
Manganese (Mn), % 4.0 to 6.0
0 to 0.050
Nickel (Ni), % 4.0 to 6.0
0
Nitrogen (N), % 0.080 to 0.2
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 3.0 to 4.0
0 to 0.25
Sulfur (S), % 0 to 0.040
0
Titanium (Ti), % 0
0 to 0.050
Zinc (Zn), % 0
0 to 0.070