MakeItFrom.com
Menu (ESC)

7108A Aluminum vs. EN 1.4982 Stainless Steel

7108A aluminum belongs to the aluminum alloys classification, while EN 1.4982 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 7108A aluminum and the bottom bar is EN 1.4982 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
200
Elongation at Break, % 11 to 13
28
Fatigue Strength, MPa 120 to 130
420
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
76
Shear Strength, MPa 210
490
Tensile Strength: Ultimate (UTS), MPa 350
750
Tensile Strength: Yield (Proof), MPa 290 to 300
570

Thermal Properties

Latent Heat of Fusion, J/g 380
290
Maximum Temperature: Mechanical, °C 210
860
Melting Completion (Liquidus), °C 630
1430
Melting Onset (Solidus), °C 520
1390
Specific Heat Capacity, J/kg-K 870
470
Thermal Conductivity, W/m-K 150
13
Thermal Expansion, µm/m-K 24
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 36
2.3
Electrical Conductivity: Equal Weight (Specific), % IACS 110
2.7

Otherwise Unclassified Properties

Base Metal Price, % relative 10
22
Density, g/cm3 2.9
7.8
Embodied Carbon, kg CO2/kg material 8.3
4.9
Embodied Energy, MJ/kg 150
71
Embodied Water, L/kg 1150
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 38 to 44
190
Resilience: Unit (Modulus of Resilience), kJ/m3 610 to 640
830
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 47
25
Strength to Weight: Axial, points 33 to 34
27
Strength to Weight: Bending, points 38
23
Thermal Diffusivity, mm2/s 59
3.4
Thermal Shock Resistance, points 15 to 16
17

Alloy Composition

Aluminum (Al), % 91.6 to 94.4
0
Boron (B), % 0
0.0030 to 0.0090
Carbon (C), % 0
0.070 to 0.13
Chromium (Cr), % 0 to 0.040
14 to 16
Copper (Cu), % 0 to 0.050
0
Gallium (Ga), % 0 to 0.030
0
Iron (Fe), % 0 to 0.3
61.8 to 69.7
Magnesium (Mg), % 0.7 to 1.5
0
Manganese (Mn), % 0 to 0.050
5.5 to 7.0
Molybdenum (Mo), % 0
0.8 to 1.2
Nickel (Ni), % 0
9.0 to 11
Niobium (Nb), % 0
0.75 to 1.3
Nitrogen (N), % 0
0 to 0.1
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.2
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.030
0
Vanadium (V), % 0
0.15 to 0.4
Zinc (Zn), % 4.8 to 5.8
0
Zirconium (Zr), % 0.15 to 0.25
0
Residuals, % 0 to 0.15
0