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AISI 305 Stainless Steel vs. 5154A Aluminum

AISI 305 stainless steel belongs to the iron alloys classification, while 5154A aluminum belongs to the aluminum 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 AISI 305 stainless steel and the bottom bar is 5154A aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 170 to 220
58 to 100
Elastic (Young's, Tensile) Modulus, GPa 200
68
Elongation at Break, % 34 to 45
1.1 to 19
Fatigue Strength, MPa 210 to 280
83 to 160
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
26
Shear Strength, MPa 400 to 470
140 to 210
Tensile Strength: Ultimate (UTS), MPa 580 to 710
230 to 370
Tensile Strength: Yield (Proof), MPa 230 to 350
96 to 320

Thermal Properties

Latent Heat of Fusion, J/g 290
400
Maximum Temperature: Mechanical, °C 540
190
Melting Completion (Liquidus), °C 1450
650
Melting Onset (Solidus), °C 1400
600
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 16
130
Thermal Expansion, µm/m-K 17
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.4
32
Electrical Conductivity: Equal Weight (Specific), % IACS 2.7
110

Otherwise Unclassified Properties

Base Metal Price, % relative 16
9.5
Density, g/cm3 7.8
2.7
Embodied Carbon, kg CO2/kg material 3.2
8.8
Embodied Energy, MJ/kg 45
150
Embodied Water, L/kg 150
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 200 to 210
4.0 to 36
Resilience: Unit (Modulus of Resilience), kJ/m3 130 to 320
68 to 760
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
51
Strength to Weight: Axial, points 20 to 25
24 to 38
Strength to Weight: Bending, points 20 to 23
31 to 43
Thermal Diffusivity, mm2/s 4.2
53
Thermal Shock Resistance, points 13 to 15
10 to 16

Alloy Composition

Aluminum (Al), % 0
93.7 to 96.9
Carbon (C), % 0 to 0.12
0
Chromium (Cr), % 17 to 19
0 to 0.25
Copper (Cu), % 0
0 to 0.1
Iron (Fe), % 65.1 to 72.5
0 to 0.5
Magnesium (Mg), % 0
3.1 to 3.9
Manganese (Mn), % 0 to 2.0
0 to 0.5
Nickel (Ni), % 10.5 to 13
0
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 0.75
0 to 0.5
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0 to 0.2
Zinc (Zn), % 0
0 to 0.2
Residuals, % 0
0 to 0.15