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A380.0 Aluminum vs. S17600 Stainless Steel

A380.0 aluminum belongs to the aluminum alloys classification, while S17600 stainless steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (5, 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 A380.0 aluminum and the bottom bar is S17600 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 80
270 to 410
Elastic (Young's, Tensile) Modulus, GPa 73
200
Elongation at Break, % 3.3
8.6 to 11
Fatigue Strength, MPa 140
300 to 680
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
76
Shear Strength, MPa 190
560 to 880
Tensile Strength: Ultimate (UTS), MPa 290
940 to 1490
Tensile Strength: Yield (Proof), MPa 160
580 to 1310

Thermal Properties

Latent Heat of Fusion, J/g 510
290
Maximum Temperature: Mechanical, °C 170
890
Melting Completion (Liquidus), °C 590
1430
Melting Onset (Solidus), °C 550
1390
Specific Heat Capacity, J/kg-K 870
480
Thermal Conductivity, W/m-K 96
15
Thermal Expansion, µm/m-K 22
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 25
2.3
Electrical Conductivity: Equal Weight (Specific), % IACS 78
2.7

Otherwise Unclassified Properties

Base Metal Price, % relative 11
13
Density, g/cm3 2.9
7.8
Embodied Carbon, kg CO2/kg material 7.5
2.9
Embodied Energy, MJ/kg 140
42
Embodied Water, L/kg 1040
130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 8.3
70 to 150
Resilience: Unit (Modulus of Resilience), kJ/m3 180
850 to 4390
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 48
25
Strength to Weight: Axial, points 28
34 to 54
Strength to Weight: Bending, points 34
28 to 37
Thermal Diffusivity, mm2/s 38
4.1
Thermal Shock Resistance, points 13
31 to 50

Alloy Composition


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Aluminum (Al), % 80.3 to 89.5
0 to 0.4
Carbon (C), % 0
0 to 0.080
Chromium (Cr), % 0
16 to 17.5
Copper (Cu), % 3.0 to 4.0
0
Iron (Fe), % 0 to 1.3
71.3 to 77.6
Magnesium (Mg), % 0 to 0.1
0
Manganese (Mn), % 0 to 0.5
0 to 1.0
Nickel (Ni), % 0 to 0.5
6.0 to 7.5
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 7.5 to 9.5
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Tin (Sn), % 0 to 0.35
0
Titanium (Ti), % 0
0.4 to 1.2
Zinc (Zn), % 0 to 3.0
0
Residuals, % 0 to 0.5
0