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S34565 Stainless Steel vs. 710.0 Aluminum

S34565 stainless steel belongs to the iron alloys classification, while 710.0 aluminum belongs to the aluminum 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 S34565 stainless steel and the bottom bar is 710.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 200
75
Elastic (Young's, Tensile) Modulus, GPa 210
70
Elongation at Break, % 39
2.2 to 3.6
Fatigue Strength, MPa 400
55 to 110
Poisson's Ratio 0.28
0.32
Shear Modulus, GPa 80
26
Shear Strength, MPa 610
180
Tensile Strength: Ultimate (UTS), MPa 900
240 to 250
Tensile Strength: Yield (Proof), MPa 470
160

Thermal Properties

Latent Heat of Fusion, J/g 310
380
Maximum Temperature: Mechanical, °C 1100
170
Melting Completion (Liquidus), °C 1420
650
Melting Onset (Solidus), °C 1380
610
Specific Heat Capacity, J/kg-K 470
870
Thermal Conductivity, W/m-K 12
140
Thermal Expansion, µm/m-K 15
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.9
35
Electrical Conductivity: Equal Weight (Specific), % IACS 2.1
110

Otherwise Unclassified Properties

Base Metal Price, % relative 28
9.5
Density, g/cm3 7.9
3.0
Embodied Carbon, kg CO2/kg material 5.3
8.0
Embodied Energy, MJ/kg 73
150
Embodied Water, L/kg 210
1130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 300
4.9 to 7.9
Resilience: Unit (Modulus of Resilience), kJ/m3 540
180 to 190
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
46
Strength to Weight: Axial, points 32
23
Strength to Weight: Bending, points 26
29
Thermal Diffusivity, mm2/s 3.2
53
Thermal Shock Resistance, points 22
10 to 11

Alloy Composition

Aluminum (Al), % 0
90.5 to 93.1
Carbon (C), % 0 to 0.030
0
Chromium (Cr), % 23 to 25
0
Copper (Cu), % 0
0.35 to 0.65
Iron (Fe), % 43.2 to 51.6
0 to 0.5
Magnesium (Mg), % 0
0.6 to 0.8
Manganese (Mn), % 5.0 to 7.0
0 to 0.050
Molybdenum (Mo), % 4.0 to 5.0
0
Nickel (Ni), % 16 to 18
0
Niobium (Nb), % 0 to 0.1
0
Nitrogen (N), % 0.4 to 0.6
0
Phosphorus (P), % 0 to 0.030
0
Silicon (Si), % 0 to 1.0
0 to 0.15
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0
0 to 0.25
Zinc (Zn), % 0
6.0 to 7.0
Residuals, % 0
0 to 0.15