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SAE-AISI D2 Steel vs. 7129 Aluminum

SAE-AISI D2 steel belongs to the iron alloys classification, while 7129 Aluminum belongs to the aluminum alloys. There are 29 material properties with values for both materials. Properties with values for just one material (2, 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 D2 steel and the bottom bar is 7129 Aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
69
Elongation at Break, % 5.0 to 16
9.0 to 9.1
Fatigue Strength, MPa 310 to 860
150 to 190
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 75
26
Shear Strength, MPa 460 to 1160
250 to 260
Tensile Strength: Ultimate (UTS), MPa 760 to 2000
430
Tensile Strength: Yield (Proof), MPa 470 to 1510
380 to 390

Thermal Properties

Latent Heat of Fusion, J/g 270
380
Melting Completion (Liquidus), °C 1440
630
Melting Onset (Solidus), °C 1390
510
Specific Heat Capacity, J/kg-K 480
880
Thermal Conductivity, W/m-K 31
150
Thermal Expansion, µm/m-K 11
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 4.3
40
Electrical Conductivity: Equal Weight (Specific), % IACS 5.1
120

Otherwise Unclassified Properties

Base Metal Price, % relative 8.0
9.5
Density, g/cm3 7.7
2.9
Embodied Carbon, kg CO2/kg material 3.4
8.3
Embodied Energy, MJ/kg 50
150
Embodied Water, L/kg 100
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 92 to 100
37 to 38
Resilience: Unit (Modulus of Resilience), kJ/m3 570 to 5940
1050 to 1090
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
47
Strength to Weight: Axial, points 27 to 72
41
Strength to Weight: Bending, points 24 to 46
43 to 44
Thermal Diffusivity, mm2/s 8.3
58
Thermal Shock Resistance, points 25 to 67
19

Alloy Composition

Aluminum (Al), % 0
91 to 94
Carbon (C), % 1.4 to 1.6
0
Chromium (Cr), % 11 to 13
0 to 0.1
Copper (Cu), % 0 to 0.25
0.5 to 0.9
Gallium (Ga), % 0
0 to 0.030
Iron (Fe), % 81.3 to 86.9
0 to 0.3
Magnesium (Mg), % 0
1.3 to 2.0
Manganese (Mn), % 0 to 0.6
0 to 0.1
Molybdenum (Mo), % 0.7 to 1.2
0
Nickel (Ni), % 0 to 0.3
0
Phosphorus (P), % 0 to 0.030
0
Silicon (Si), % 0 to 0.6
0 to 0.15
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0 to 0.050
Vanadium (V), % 0 to 1.1
0 to 0.050
Zinc (Zn), % 0
4.2 to 5.2
Residuals, % 0
0 to 0.15