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7005 Aluminum vs. EN 1.4568 Stainless Steel

7005 aluminum belongs to the aluminum alloys classification, while EN 1.4568 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, 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 1.4568 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
200
Elongation at Break, % 10 to 20
2.3 to 21
Fatigue Strength, MPa 100 to 190
220 to 670
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
76
Shear Strength, MPa 120 to 230
520 to 930
Tensile Strength: Ultimate (UTS), MPa 200 to 400
830 to 1620
Tensile Strength: Yield (Proof), MPa 95 to 350
330 to 1490

Thermal Properties

Latent Heat of Fusion, J/g 380
280
Maximum Temperature: Mechanical, °C 200
890
Melting Completion (Liquidus), °C 640
1420
Melting Onset (Solidus), °C 610
1380
Specific Heat Capacity, J/kg-K 880
480
Thermal Conductivity, W/m-K 140 to 170
16
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35 to 43
2.2
Electrical Conductivity: Equal Weight (Specific), % IACS 110 to 130
2.5

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
13
Density, g/cm3 2.9
7.7
Embodied Carbon, kg CO2/kg material 8.3
2.8
Embodied Energy, MJ/kg 150
40
Embodied Water, L/kg 1150
140

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 32 to 57
36 to 140
Resilience: Unit (Modulus of Resilience), kJ/m3 65 to 850
290 to 5710
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 47
25
Strength to Weight: Axial, points 19 to 38
30 to 58
Strength to Weight: Bending, points 26 to 41
25 to 40
Thermal Diffusivity, mm2/s 54 to 65
4.3
Thermal Shock Resistance, points 8.7 to 18
23 to 46

Alloy Composition

Aluminum (Al), % 91 to 94.7
0.7 to 1.5
Carbon (C), % 0
0 to 0.090
Chromium (Cr), % 0.060 to 0.2
16 to 18
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.4
70.9 to 76.8
Magnesium (Mg), % 1.0 to 1.8
0
Manganese (Mn), % 0.2 to 0.7
0 to 1.0
Nickel (Ni), % 0
6.5 to 7.8
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.35
0 to 0.7
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