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772.0 Aluminum vs. S66286 Stainless Steel

772.0 aluminum belongs to the aluminum alloys classification, while S66286 stainless steel belongs to the iron alloys. There are 29 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 772.0 aluminum and the bottom bar is S66286 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
190
Elongation at Break, % 6.3 to 8.4
17 to 40
Fatigue Strength, MPa 94 to 160
240 to 410
Poisson's Ratio 0.32
0.29
Shear Modulus, GPa 26
75
Tensile Strength: Ultimate (UTS), MPa 260 to 320
620 to 1020
Tensile Strength: Yield (Proof), MPa 220 to 250
280 to 670

Thermal Properties

Latent Heat of Fusion, J/g 380
300
Maximum Temperature: Mechanical, °C 180
920
Melting Completion (Liquidus), °C 630
1430
Melting Onset (Solidus), °C 580
1370
Specific Heat Capacity, J/kg-K 870
470
Thermal Conductivity, W/m-K 150
15
Thermal Expansion, µm/m-K 24
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
1.9
Electrical Conductivity: Equal Weight (Specific), % IACS 110
2.2

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
26
Density, g/cm3 3.0
7.9
Embodied Carbon, kg CO2/kg material 8.0
6.0
Embodied Energy, MJ/kg 150
87
Embodied Water, L/kg 1140
170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 16 to 25
150 to 200
Resilience: Unit (Modulus of Resilience), kJ/m3 350 to 430
190 to 1150
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 46
24
Strength to Weight: Axial, points 25 to 31
22 to 36
Strength to Weight: Bending, points 31 to 36
20 to 28
Thermal Diffusivity, mm2/s 58
4.0
Thermal Shock Resistance, points 11 to 14
13 to 22

Alloy Composition

Aluminum (Al), % 91.2 to 93.2
0 to 0.35
Boron (B), % 0
0.0010 to 0.010
Carbon (C), % 0
0 to 0.080
Chromium (Cr), % 0.060 to 0.2
13.5 to 16
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.15
49.1 to 59.5
Magnesium (Mg), % 0.6 to 0.8
0
Manganese (Mn), % 0 to 0.1
0 to 2.0
Molybdenum (Mo), % 0
1.0 to 1.5
Nickel (Ni), % 0
24 to 27
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.15
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0.1 to 0.2
1.9 to 2.4
Vanadium (V), % 0
0.1 to 0.5
Zinc (Zn), % 6.0 to 7.0
0
Residuals, % 0 to 0.15
0