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710.0 Aluminum vs. S44660 Stainless Steel

710.0 aluminum belongs to the aluminum alloys classification, while S44660 stainless steel belongs to the iron 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 710.0 aluminum and the bottom bar is S44660 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 75
210
Elastic (Young's, Tensile) Modulus, GPa 70
210
Elongation at Break, % 2.2 to 3.6
20
Fatigue Strength, MPa 55 to 110
330
Poisson's Ratio 0.32
0.27
Shear Modulus, GPa 26
81
Shear Strength, MPa 180
410
Tensile Strength: Ultimate (UTS), MPa 240 to 250
660
Tensile Strength: Yield (Proof), MPa 160
510

Thermal Properties

Latent Heat of Fusion, J/g 380
300
Maximum Temperature: Mechanical, °C 170
1100
Melting Completion (Liquidus), °C 650
1460
Melting Onset (Solidus), °C 610
1410
Specific Heat Capacity, J/kg-K 870
480
Thermal Conductivity, W/m-K 140
17
Thermal Expansion, µm/m-K 24
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
2.5
Electrical Conductivity: Equal Weight (Specific), % IACS 110
2.9

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
21
Density, g/cm3 3.0
7.7
Embodied Carbon, kg CO2/kg material 8.0
4.3
Embodied Energy, MJ/kg 150
61
Embodied Water, L/kg 1130
180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.9 to 7.9
120
Resilience: Unit (Modulus of Resilience), kJ/m3 180 to 190
640
Stiffness to Weight: Axial, points 13
15
Stiffness to Weight: Bending, points 46
25
Strength to Weight: Axial, points 23
24
Strength to Weight: Bending, points 29
22
Thermal Diffusivity, mm2/s 53
4.5
Thermal Shock Resistance, points 10 to 11
21

Alloy Composition

Aluminum (Al), % 90.5 to 93.1
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0
25 to 28
Copper (Cu), % 0.35 to 0.65
0
Iron (Fe), % 0 to 0.5
60.4 to 71
Magnesium (Mg), % 0.6 to 0.8
0
Manganese (Mn), % 0 to 0.050
0 to 1.0
Molybdenum (Mo), % 0
3.0 to 4.0
Nickel (Ni), % 0
1.0 to 3.5
Niobium (Nb), % 0
0.2 to 1.0
Nitrogen (N), % 0
0 to 0.040
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 to 0.25
0.2 to 1.0
Zinc (Zn), % 6.0 to 7.0
0
Residuals, % 0 to 0.15
0