MakeItFrom.com
Menu (ESC)

5005 Aluminum vs. EN 1.7390 Steel

5005 aluminum belongs to the aluminum alloys classification, while EN 1.7390 steel belongs to the iron alloys. There are 31 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 5005 aluminum and the bottom bar is EN 1.7390 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 28 to 64
210
Elastic (Young's, Tensile) Modulus, GPa 68
190
Elongation at Break, % 1.1 to 23
16
Fatigue Strength, MPa 38 to 86
310
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
74
Shear Strength, MPa 70 to 130
440
Tensile Strength: Ultimate (UTS), MPa 110 to 230
710
Tensile Strength: Yield (Proof), MPa 41 to 210
480

Thermal Properties

Latent Heat of Fusion, J/g 400
260
Maximum Temperature: Mechanical, °C 180
510
Melting Completion (Liquidus), °C 650
1460
Melting Onset (Solidus), °C 630
1420
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 200
40
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 52
8.1
Electrical Conductivity: Equal Weight (Specific), % IACS 170
9.3

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
4.3
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 8.3
1.7
Embodied Energy, MJ/kg 150
23
Embodied Water, L/kg 1190
69

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.3 to 22
100
Resilience: Unit (Modulus of Resilience), kJ/m3 12 to 320
600
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 11 to 23
25
Strength to Weight: Bending, points 19 to 31
23
Thermal Diffusivity, mm2/s 82
11
Thermal Shock Resistance, points 4.9 to 10
20

Alloy Composition

Aluminum (Al), % 97 to 99.5
0
Carbon (C), % 0
0 to 0.18
Chromium (Cr), % 0 to 0.1
4.0 to 6.0
Copper (Cu), % 0 to 0.2
0
Iron (Fe), % 0 to 0.7
91.9 to 95.3
Magnesium (Mg), % 0.5 to 1.1
0
Manganese (Mn), % 0 to 0.2
0.3 to 0.8
Molybdenum (Mo), % 0
0.45 to 0.65
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.3
0 to 0.4
Sulfur (S), % 0
0 to 0.015
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0