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3102 Aluminum vs. EN 1.4107 Stainless Steel

3102 aluminum belongs to the aluminum alloys classification, while EN 1.4107 stainless steel belongs to the iron alloys. There are 29 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 3102 aluminum and the bottom bar is EN 1.4107 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
190
Elongation at Break, % 23 to 28
18 to 21
Fatigue Strength, MPa 31 to 34
260 to 350
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
76
Tensile Strength: Ultimate (UTS), MPa 92 to 100
620 to 700
Tensile Strength: Yield (Proof), MPa 28 to 34
400 to 570

Thermal Properties

Latent Heat of Fusion, J/g 400
270
Maximum Temperature: Mechanical, °C 180
740
Melting Completion (Liquidus), °C 640
1450
Melting Onset (Solidus), °C 640
1410
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 230
27
Thermal Expansion, µm/m-K 23
10

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 56
2.9
Electrical Conductivity: Equal Weight (Specific), % IACS 190
3.3

Otherwise Unclassified Properties

Base Metal Price, % relative 9.0
7.5
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 8.2
2.1
Embodied Energy, MJ/kg 150
30
Embodied Water, L/kg 1190
100

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 16 to 22
110 to 120
Resilience: Unit (Modulus of Resilience), kJ/m3 5.8 to 8.3
420 to 840
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 9.4 to 10
22 to 25
Strength to Weight: Bending, points 17 to 18
21 to 22
Thermal Diffusivity, mm2/s 92
7.2
Thermal Shock Resistance, points 4.1 to 4.4
22 to 25

Alloy Composition


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Aluminum (Al), % 97.9 to 99.95
0
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0
11.5 to 12.5
Copper (Cu), % 0 to 0.1
0 to 0.3
Iron (Fe), % 0 to 0.7
83.8 to 87.2
Manganese (Mn), % 0.050 to 0.4
0.5 to 0.8
Molybdenum (Mo), % 0
0 to 0.5
Nickel (Ni), % 0
0.8 to 1.5
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 0.4
0 to 0.4
Sulfur (S), % 0
0 to 0.020
Titanium (Ti), % 0 to 0.1
0
Vanadium (V), % 0
0 to 0.080
Zinc (Zn), % 0 to 0.3
0
Residuals, % 0 to 0.15
0

Comparable Variants