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SAE-AISI D2 Steel vs. 6025 Aluminum

SAE-AISI D2 steel belongs to the iron alloys classification, while 6025 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 6025 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
70
Elongation at Break, % 5.0 to 16
2.8 to 10
Fatigue Strength, MPa 310 to 860
67 to 110
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 75
26
Shear Strength, MPa 460 to 1160
110 to 140
Tensile Strength: Ultimate (UTS), MPa 760 to 2000
190 to 240
Tensile Strength: Yield (Proof), MPa 470 to 1510
68 to 210

Thermal Properties

Latent Heat of Fusion, J/g 270
410
Melting Completion (Liquidus), °C 1440
650
Melting Onset (Solidus), °C 1390
550
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 31
130
Thermal Expansion, µm/m-K 11
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 4.3
33
Electrical Conductivity: Equal Weight (Specific), % IACS 5.1
110

Otherwise Unclassified Properties

Base Metal Price, % relative 8.0
9.5
Density, g/cm3 7.7
2.8
Embodied Carbon, kg CO2/kg material 3.4
8.5
Embodied Energy, MJ/kg 50
150
Embodied Water, L/kg 100
1160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 92 to 100
6.0 to 15
Resilience: Unit (Modulus of Resilience), kJ/m3 570 to 5940
33 to 310
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 27 to 72
19 to 24
Strength to Weight: Bending, points 24 to 46
26 to 31
Thermal Diffusivity, mm2/s 8.3
54
Thermal Shock Resistance, points 25 to 67
8.2 to 10

Alloy Composition

Aluminum (Al), % 0
91.7 to 96.3
Carbon (C), % 1.4 to 1.6
0
Chromium (Cr), % 11 to 13
0 to 0.2
Copper (Cu), % 0 to 0.25
0.2 to 0.7
Iron (Fe), % 81.3 to 86.9
0 to 0.7
Magnesium (Mg), % 0
2.1 to 3.0
Manganese (Mn), % 0 to 0.6
0.6 to 1.4
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
0.8 to 1.5
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0 to 0.2
Vanadium (V), % 0 to 1.1
0
Zinc (Zn), % 0
0 to 0.5
Residuals, % 0
0 to 0.15

Comparable Variants