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7005 Aluminum vs. EN 1.4567 Stainless Steel

7005 aluminum belongs to the aluminum alloys classification, while EN 1.4567 stainless steel belongs to the iron alloys. There are 30 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 7005 aluminum and the bottom bar is EN 1.4567 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
190
Elongation at Break, % 10 to 20
22 to 51
Fatigue Strength, MPa 100 to 190
190 to 260
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
76
Shear Strength, MPa 120 to 230
390 to 490
Tensile Strength: Ultimate (UTS), MPa 200 to 400
550 to 780
Tensile Strength: Yield (Proof), MPa 95 to 350
200 to 390

Thermal Properties

Latent Heat of Fusion, J/g 380
290
Maximum Temperature: Mechanical, °C 200
930
Melting Completion (Liquidus), °C 640
1410
Melting Onset (Solidus), °C 610
1370
Specific Heat Capacity, J/kg-K 880
480
Thermal Conductivity, W/m-K 140 to 170
11
Thermal Expansion, µm/m-K 23
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35 to 43
2.4
Electrical Conductivity: Equal Weight (Specific), % IACS 110 to 130
2.7

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
16
Density, g/cm3 2.9
7.8
Embodied Carbon, kg CO2/kg material 8.3
3.1
Embodied Energy, MJ/kg 150
43
Embodied Water, L/kg 1150
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 32 to 57
150 to 220
Resilience: Unit (Modulus of Resilience), kJ/m3 65 to 850
100 to 400
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 47
25
Strength to Weight: Axial, points 19 to 38
19 to 27
Strength to Weight: Bending, points 26 to 41
19 to 24
Thermal Diffusivity, mm2/s 54 to 65
3.0
Thermal Shock Resistance, points 8.7 to 18
12 to 17

Alloy Composition

Aluminum (Al), % 91 to 94.7
0
Carbon (C), % 0
0 to 0.040
Chromium (Cr), % 0.060 to 0.2
17 to 19
Copper (Cu), % 0 to 0.1
3.0 to 4.0
Iron (Fe), % 0 to 0.4
63.3 to 71.5
Magnesium (Mg), % 1.0 to 1.8
0
Manganese (Mn), % 0.2 to 0.7
0 to 2.0
Nickel (Ni), % 0
8.5 to 10.5
Nitrogen (N), % 0
0 to 0.1
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0 to 0.35
0 to 1.0
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0.010 to 0.060
0
Zinc (Zn), % 4.0 to 5.0
0
Zirconium (Zr), % 0.080 to 0.2
0
Residuals, % 0 to 0.15
0