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7005 Aluminum vs. EN 1.4418 Stainless Steel

7005 aluminum belongs to the aluminum alloys classification, while EN 1.4418 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (4, 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 1.4418 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
200
Elongation at Break, % 10 to 20
16 to 20
Fatigue Strength, MPa 100 to 190
350 to 480
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
77
Shear Strength, MPa 120 to 230
530 to 620
Tensile Strength: Ultimate (UTS), MPa 200 to 400
860 to 1000
Tensile Strength: Yield (Proof), MPa 95 to 350
540 to 790

Thermal Properties

Latent Heat of Fusion, J/g 380
280
Maximum Temperature: Mechanical, °C 200
870
Melting Completion (Liquidus), °C 640
1450
Melting Onset (Solidus), °C 610
1400
Specific Heat Capacity, J/kg-K 880
480
Thermal Conductivity, W/m-K 140 to 170
15
Thermal Expansion, µm/m-K 23
10

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
7.8
Embodied Carbon, kg CO2/kg material 8.3
2.8
Embodied Energy, MJ/kg 150
39
Embodied Water, L/kg 1150
130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 32 to 57
130 to 170
Resilience: Unit (Modulus of Resilience), kJ/m3 65 to 850
730 to 1590
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 47
25
Strength to Weight: Axial, points 19 to 38
31 to 36
Strength to Weight: Bending, points 26 to 41
26 to 28
Thermal Diffusivity, mm2/s 54 to 65
4.0
Thermal Shock Resistance, points 8.7 to 18
31 to 36

Alloy Composition

Aluminum (Al), % 91 to 94.7
0
Carbon (C), % 0
0 to 0.060
Chromium (Cr), % 0.060 to 0.2
15 to 17
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.4
73.2 to 80.2
Magnesium (Mg), % 1.0 to 1.8
0
Manganese (Mn), % 0.2 to 0.7
0 to 1.5
Molybdenum (Mo), % 0
0.8 to 1.5
Nickel (Ni), % 0
4.0 to 6.0
Nitrogen (N), % 0
0 to 0.020
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

Comparable Variants