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S44627 Stainless Steel vs. 1200 Aluminum

S44627 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 S44627 stainless steel and the bottom bar is 1200 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 170
23 to 48
Elastic (Young's, Tensile) Modulus, GPa 200
69
Elongation at Break, % 24
1.1 to 28
Fatigue Strength, MPa 200
25 to 69
Poisson's Ratio 0.27
0.33
Shear Modulus, GPa 80
26
Shear Strength, MPa 310
54 to 100
Tensile Strength: Ultimate (UTS), MPa 490
85 to 180
Tensile Strength: Yield (Proof), MPa 300
28 to 160

Thermal Properties

Latent Heat of Fusion, J/g 290
400
Maximum Temperature: Mechanical, °C 1100
170
Melting Completion (Liquidus), °C 1440
660
Melting Onset (Solidus), °C 1400
650
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 17
230
Thermal Expansion, µm/m-K 11
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.2
58
Electrical Conductivity: Equal Weight (Specific), % IACS 2.6
190

Otherwise Unclassified Properties

Base Metal Price, % relative 14
9.0
Density, g/cm3 7.7
2.7
Embodied Carbon, kg CO2/kg material 2.9
8.2
Embodied Energy, MJ/kg 41
150
Embodied Water, L/kg 160
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 100
2.0 to 19
Resilience: Unit (Modulus of Resilience), kJ/m3 220
5.7 to 180
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 18
8.7 to 19
Strength to Weight: Bending, points 18
16 to 26
Thermal Diffusivity, mm2/s 4.6
92
Thermal Shock Resistance, points 16
3.8 to 8.1

Alloy Composition

Aluminum (Al), % 0
99 to 100
Carbon (C), % 0 to 0.010
0
Chromium (Cr), % 25 to 27.5
0
Copper (Cu), % 0 to 0.2
0 to 0.050
Iron (Fe), % 69.2 to 74.2
0 to 1.0
Manganese (Mn), % 0 to 0.4
0 to 0.050
Molybdenum (Mo), % 0.75 to 1.5
0
Nickel (Ni), % 0 to 0.5
0
Niobium (Nb), % 0.050 to 0.2
0
Nitrogen (N), % 0 to 0.015
0
Phosphorus (P), % 0 to 0.020
0
Silicon (Si), % 0 to 0.4
0 to 1.0
Sulfur (S), % 0 to 0.020
0
Titanium (Ti), % 0
0 to 0.050
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15