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N08367 Stainless Steel vs. 1200 Aluminum

N08367 stainless steel belongs to the iron alloys classification, while 1200 aluminum belongs to the aluminum alloys. There are 31 material properties with values for both materials. Properties with values for just one material (4, 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 N08367 stainless steel and the bottom bar is 1200 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 210
23 to 48
Elastic (Young's, Tensile) Modulus, GPa 210
69
Elongation at Break, % 34
1.1 to 28
Fatigue Strength, MPa 280
25 to 69
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 80
26
Shear Strength, MPa 490
54 to 100
Tensile Strength: Ultimate (UTS), MPa 740
85 to 180
Tensile Strength: Yield (Proof), MPa 350
28 to 160

Thermal Properties

Latent Heat of Fusion, J/g 310
400
Maximum Temperature: Mechanical, °C 1100
170
Melting Completion (Liquidus), °C 1460
660
Melting Onset (Solidus), °C 1410
650
Specific Heat Capacity, J/kg-K 460
900
Thermal Conductivity, W/m-K 12
230
Thermal Expansion, µm/m-K 15
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.8
58
Electrical Conductivity: Equal Weight (Specific), % IACS 2.0
190

Otherwise Unclassified Properties

Base Metal Price, % relative 33
9.0
Density, g/cm3 8.1
2.7
Embodied Carbon, kg CO2/kg material 6.2
8.2
Embodied Energy, MJ/kg 84
150
Embodied Water, L/kg 200
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 210
2.0 to 19
Resilience: Unit (Modulus of Resilience), kJ/m3 290
5.7 to 180
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 24
50
Strength to Weight: Axial, points 25
8.7 to 19
Strength to Weight: Bending, points 22
16 to 26
Thermal Diffusivity, mm2/s 3.2
92
Thermal Shock Resistance, points 17
3.8 to 8.1

Alloy Composition


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Aluminum (Al), % 0
99 to 100
Carbon (C), % 0 to 0.030
0
Chromium (Cr), % 20 to 22
0
Copper (Cu), % 0 to 0.75
0 to 0.050
Iron (Fe), % 41.4 to 50.3
0 to 1.0
Manganese (Mn), % 0 to 2.0
0 to 0.050
Molybdenum (Mo), % 6.0 to 7.0
0
Nickel (Ni), % 23.5 to 25.5
0
Nitrogen (N), % 0.18 to 0.25
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0 to 1.0
0 to 1.0
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0 to 0.050
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15