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7475 Aluminum vs. SAE-AISI D2 Steel

7475 aluminum belongs to the aluminum alloys classification, while SAE-AISI D2 steel belongs to the iron 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 7475 aluminum and the bottom bar is SAE-AISI D2 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
190
Elongation at Break, % 10 to 12
5.0 to 16
Fatigue Strength, MPa 190 to 210
310 to 860
Poisson's Ratio 0.32
0.28
Shear Modulus, GPa 26
75
Shear Strength, MPa 320 to 350
460 to 1160
Tensile Strength: Ultimate (UTS), MPa 530 to 590
760 to 2000
Tensile Strength: Yield (Proof), MPa 440 to 520
470 to 1510

Thermal Properties

Latent Heat of Fusion, J/g 380
270
Melting Completion (Liquidus), °C 640
1440
Melting Onset (Solidus), °C 480
1390
Specific Heat Capacity, J/kg-K 870
480
Thermal Conductivity, W/m-K 140 to 160
31
Thermal Expansion, µm/m-K 23
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 33 to 42
4.3
Electrical Conductivity: Equal Weight (Specific), % IACS 98 to 120
5.1

Otherwise Unclassified Properties

Base Metal Price, % relative 10
8.0
Density, g/cm3 3.0
7.7
Embodied Carbon, kg CO2/kg material 8.2
3.4
Embodied Energy, MJ/kg 150
50
Embodied Water, L/kg 1130
100

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 53 to 68
92 to 100
Resilience: Unit (Modulus of Resilience), kJ/m3 1390 to 1920
570 to 5940
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 46
25
Strength to Weight: Axial, points 49 to 55
27 to 72
Strength to Weight: Bending, points 48 to 52
24 to 46
Thermal Diffusivity, mm2/s 53 to 63
8.3
Thermal Shock Resistance, points 23 to 26
25 to 67

Alloy Composition

Aluminum (Al), % 88.6 to 91.6
0
Carbon (C), % 0
1.4 to 1.6
Chromium (Cr), % 0.18 to 0.25
11 to 13
Copper (Cu), % 1.2 to 1.9
0 to 0.25
Iron (Fe), % 0 to 0.12
81.3 to 86.9
Magnesium (Mg), % 1.9 to 2.6
0
Manganese (Mn), % 0 to 0.060
0 to 0.6
Molybdenum (Mo), % 0
0.7 to 1.2
Nickel (Ni), % 0
0 to 0.3
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 0.1
0 to 0.6
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.060
0
Vanadium (V), % 0
0 to 1.1
Zinc (Zn), % 5.1 to 6.2
0
Residuals, % 0 to 0.15
0