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512.0 Aluminum vs. AISI 410 Stainless Steel

512.0 aluminum belongs to the aluminum alloys classification, while AISI 410 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (5, 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 512.0 aluminum and the bottom bar is AISI 410 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 50
190 to 240
Elastic (Young's, Tensile) Modulus, GPa 69
190
Elongation at Break, % 2.0
16 to 22
Fatigue Strength, MPa 58
190 to 350
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
76
Tensile Strength: Ultimate (UTS), MPa 130
520 to 770
Tensile Strength: Yield (Proof), MPa 83
290 to 580

Thermal Properties

Latent Heat of Fusion, J/g 420
270
Maximum Temperature: Mechanical, °C 180
710
Melting Completion (Liquidus), °C 630
1530
Melting Onset (Solidus), °C 590
1480
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 150
30
Thermal Expansion, µm/m-K 23
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 38
2.9
Electrical Conductivity: Equal Weight (Specific), % IACS 130
3.3

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
7.0
Density, g/cm3 2.7
7.7
Embodied Carbon, kg CO2/kg material 8.8
1.9
Embodied Energy, MJ/kg 150
27
Embodied Water, L/kg 1160
100

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.3
97 to 110
Resilience: Unit (Modulus of Resilience), kJ/m3 50
210 to 860
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
25
Strength to Weight: Axial, points 14
19 to 28
Strength to Weight: Bending, points 22
19 to 24
Thermal Diffusivity, mm2/s 60
8.1
Thermal Shock Resistance, points 6.1
18 to 26

Alloy Composition

Aluminum (Al), % 90.6 to 95.1
0
Carbon (C), % 0
0.080 to 0.15
Chromium (Cr), % 0 to 0.25
11.5 to 13.5
Copper (Cu), % 0 to 0.35
0
Iron (Fe), % 0 to 0.6
83.5 to 88.4
Magnesium (Mg), % 3.5 to 4.5
0
Manganese (Mn), % 0 to 0.8
0 to 1.0
Nickel (Ni), % 0
0 to 0.75
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 1.4 to 2.2
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 0 to 0.35
0
Residuals, % 0 to 0.15
0