MakeItFrom.com
Menu (ESC)

AISI 305 Stainless Steel vs. 5083 Aluminum

AISI 305 stainless steel belongs to the iron alloys classification, while 5083 aluminum belongs to the aluminum alloys. There are 33 material properties with values for both materials. Properties with values for just one material (1, 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 5083 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 170 to 220
75 to 110
Elastic (Young's, Tensile) Modulus, GPa 200
68
Elongation at Break, % 34 to 45
1.1 to 17
Fatigue Strength, MPa 210 to 280
93 to 190
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
26
Shear Strength, MPa 400 to 470
170 to 220
Tensile Strength: Ultimate (UTS), MPa 580 to 710
290 to 390
Tensile Strength: Yield (Proof), MPa 230 to 350
110 to 340

Thermal Properties

Latent Heat of Fusion, J/g 290
400
Maximum Temperature: Corrosion, °C 410
65
Maximum Temperature: Mechanical, °C 540
190
Melting Completion (Liquidus), °C 1450
640
Melting Onset (Solidus), °C 1400
580
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 16
120
Thermal Expansion, µm/m-K 17
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.4
29
Electrical Conductivity: Equal Weight (Specific), % IACS 2.7
96

Otherwise Unclassified Properties

Base Metal Price, % relative 16
9.5
Calomel Potential, mV -70
-780
Density, g/cm3 7.8
2.7
Embodied Carbon, kg CO2/kg material 3.2
8.9
Embodied Energy, MJ/kg 45
150
Embodied Water, L/kg 150
1170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 200 to 210
4.2 to 42
Resilience: Unit (Modulus of Resilience), kJ/m3 130 to 320
95 to 860
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 20 to 25
29 to 40
Strength to Weight: Bending, points 20 to 23
36 to 44
Thermal Diffusivity, mm2/s 4.2
48
Thermal Shock Resistance, points 13 to 15
12 to 17

Alloy Composition

Aluminum (Al), % 0
92.4 to 95.6
Carbon (C), % 0 to 0.12
0
Chromium (Cr), % 17 to 19
0.050 to 0.25
Copper (Cu), % 0
0 to 0.1
Iron (Fe), % 65.1 to 72.5
0 to 0.4
Magnesium (Mg), % 0
4.0 to 4.9
Manganese (Mn), % 0 to 2.0
0.4 to 1.0
Nickel (Ni), % 10.5 to 13
0
Phosphorus (P), % 0 to 0.045
0
Silicon (Si), % 0 to 0.75
0 to 0.4
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0 to 0.15
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15