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SAE-AISI 52100 Steel vs. 7108A Aluminum

SAE-AISI 52100 steel belongs to the iron alloys classification, while 7108A aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (1, 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 SAE-AISI 52100 steel and the bottom bar is 7108A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
69
Elongation at Break, % 10 to 20
11 to 13
Fatigue Strength, MPa 250 to 340
120 to 130
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 72
26
Shear Strength, MPa 370 to 420
210
Tensile Strength: Ultimate (UTS), MPa 590 to 2010
350
Tensile Strength: Yield (Proof), MPa 360 to 560
290 to 300

Thermal Properties

Latent Heat of Fusion, J/g 250
380
Maximum Temperature: Mechanical, °C 430
210
Melting Completion (Liquidus), °C 1450
630
Melting Onset (Solidus), °C 1410
520
Specific Heat Capacity, J/kg-K 470
870
Thermal Conductivity, W/m-K 47
150
Thermal Expansion, µm/m-K 12 to 13
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.3
36
Electrical Conductivity: Equal Weight (Specific), % IACS 8.5
110

Otherwise Unclassified Properties

Base Metal Price, % relative 2.4
10
Density, g/cm3 7.8
2.9
Embodied Carbon, kg CO2/kg material 1.5
8.3
Embodied Energy, MJ/kg 20
150
Embodied Water, L/kg 51
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 54 to 310
38 to 44
Resilience: Unit (Modulus of Resilience), kJ/m3 350 to 840
610 to 640
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 24
47
Strength to Weight: Axial, points 21 to 72
33 to 34
Strength to Weight: Bending, points 20 to 45
38
Thermal Diffusivity, mm2/s 13
59
Thermal Shock Resistance, points 19 to 61
15 to 16

Alloy Composition

Aluminum (Al), % 0
91.6 to 94.4
Carbon (C), % 0.93 to 1.1
0
Chromium (Cr), % 1.4 to 1.6
0 to 0.040
Copper (Cu), % 0
0 to 0.050
Gallium (Ga), % 0
0 to 0.030
Iron (Fe), % 96.5 to 97.3
0 to 0.3
Magnesium (Mg), % 0
0.7 to 1.5
Manganese (Mn), % 0.25 to 0.45
0 to 0.050
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0.15 to 0.35
0 to 0.2
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0
0 to 0.030
Zinc (Zn), % 0
4.8 to 5.8
Zirconium (Zr), % 0
0.15 to 0.25
Residuals, % 0
0 to 0.15