MakeItFrom.com
Menu (ESC)

3104 Aluminum vs. EN 1.4542 Stainless Steel

3104 aluminum belongs to the aluminum alloys classification, while EN 1.4542 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (2, 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 3104 aluminum and the bottom bar is EN 1.4542 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
190
Elongation at Break, % 1.1 to 20
5.7 to 20
Fatigue Strength, MPa 74 to 130
370 to 640
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
76
Shear Strength, MPa 110 to 180
550 to 860
Tensile Strength: Ultimate (UTS), MPa 170 to 310
880 to 1470
Tensile Strength: Yield (Proof), MPa 68 to 270
580 to 1300

Thermal Properties

Latent Heat of Fusion, J/g 400
280
Maximum Temperature: Mechanical, °C 180
860
Melting Completion (Liquidus), °C 650
1430
Melting Onset (Solidus), °C 600
1380
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 160
16
Thermal Expansion, µm/m-K 23
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 41
2.4
Electrical Conductivity: Equal Weight (Specific), % IACS 130
2.8

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
13
Density, g/cm3 2.8
7.8
Embodied Carbon, kg CO2/kg material 8.4
2.7
Embodied Energy, MJ/kg 150
39
Embodied Water, L/kg 1180
130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 1.6 to 60
62 to 160
Resilience: Unit (Modulus of Resilience), kJ/m3 34 to 540
880 to 4360
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 17 to 31
31 to 52
Strength to Weight: Bending, points 25 to 37
26 to 37
Thermal Diffusivity, mm2/s 64
4.3
Thermal Shock Resistance, points 7.6 to 13
29 to 49

Alloy Composition

Aluminum (Al), % 95.1 to 98.4
0
Carbon (C), % 0
0 to 0.070
Chromium (Cr), % 0
15 to 17
Copper (Cu), % 0.050 to 0.25
3.0 to 5.0
Gallium (Ga), % 0 to 0.050
0
Iron (Fe), % 0 to 0.8
69.6 to 79
Magnesium (Mg), % 0.8 to 1.3
0
Manganese (Mn), % 0.8 to 1.4
0 to 1.5
Molybdenum (Mo), % 0
0 to 0.6
Nickel (Ni), % 0
3.0 to 5.0
Niobium (Nb), % 0
0 to 0.45
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.6
0 to 0.7
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.1
0
Vanadium (V), % 0 to 0.050
0
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0