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1200 Aluminum vs. S44535 Stainless Steel

1200 aluminum belongs to the aluminum alloys classification, while S44535 stainless steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (3, 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 1200 aluminum and the bottom bar is S44535 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 23 to 48
170
Elastic (Young's, Tensile) Modulus, GPa 69
200
Elongation at Break, % 1.1 to 28
28
Fatigue Strength, MPa 25 to 69
210
Poisson's Ratio 0.33
0.27
Shear Modulus, GPa 26
78
Shear Strength, MPa 54 to 100
290
Tensile Strength: Ultimate (UTS), MPa 85 to 180
450
Tensile Strength: Yield (Proof), MPa 28 to 160
290

Thermal Properties

Latent Heat of Fusion, J/g 400
290
Maximum Temperature: Mechanical, °C 170
1000
Melting Completion (Liquidus), °C 660
1430
Melting Onset (Solidus), °C 650
1390
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 230
21
Thermal Expansion, µm/m-K 23
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 58
2.6
Electrical Conductivity: Equal Weight (Specific), % IACS 190
3.1

Otherwise Unclassified Properties

Base Metal Price, % relative 9.0
11
Density, g/cm3 2.7
7.7
Embodied Carbon, kg CO2/kg material 8.2
2.4
Embodied Energy, MJ/kg 150
34
Embodied Water, L/kg 1190
140

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.0 to 19
110
Resilience: Unit (Modulus of Resilience), kJ/m3 5.7 to 180
200
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 8.7 to 19
16
Strength to Weight: Bending, points 16 to 26
17
Thermal Diffusivity, mm2/s 92
5.6
Thermal Shock Resistance, points 3.8 to 8.1
15

Alloy Composition


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Aluminum (Al), % 99 to 100
0 to 0.5
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0
20 to 24
Copper (Cu), % 0 to 0.050
0 to 0.5
Iron (Fe), % 0 to 1.0
73.2 to 79.6
Lanthanum (La), % 0
0.040 to 0.2
Manganese (Mn), % 0 to 0.050
0.3 to 0.8
Phosphorus (P), % 0
0 to 0.050
Silicon (Si), % 0 to 1.0
0 to 0.5
Sulfur (S), % 0
0 to 0.020
Titanium (Ti), % 0 to 0.050
0.030 to 0.2
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0 to 0.15
0