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AISI 301LN Stainless Steel vs. 1200 Aluminum

AISI 301LN 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 (2, 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 301LN stainless steel and the bottom bar is 1200 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 210 to 320
23 to 48
Elastic (Young's, Tensile) Modulus, GPa 200
69
Elongation at Break, % 23 to 51
1.1 to 28
Fatigue Strength, MPa 270 to 520
25 to 69
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
26
Shear Strength, MPa 450 to 670
54 to 100
Tensile Strength: Ultimate (UTS), MPa 630 to 1060
85 to 180
Tensile Strength: Yield (Proof), MPa 270 to 770
28 to 160

Thermal Properties

Latent Heat of Fusion, J/g 280
400
Maximum Temperature: Mechanical, °C 890
170
Melting Completion (Liquidus), °C 1430
660
Melting Onset (Solidus), °C 1380
650
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 15
230
Thermal Expansion, µm/m-K 16
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.4
58
Electrical Conductivity: Equal Weight (Specific), % IACS 2.7
190

Otherwise Unclassified Properties

Base Metal Price, % relative 13
9.0
Density, g/cm3 7.8
2.7
Embodied Carbon, kg CO2/kg material 2.7
8.2
Embodied Energy, MJ/kg 39
150
Embodied Water, L/kg 130
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 220 to 290
2.0 to 19
Resilience: Unit (Modulus of Resilience), kJ/m3 180 to 1520
5.7 to 180
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 22 to 38
8.7 to 19
Strength to Weight: Bending, points 21 to 30
16 to 26
Thermal Diffusivity, mm2/s 4.0
92
Thermal Shock Resistance, points 14 to 24
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), % 16 to 18
0
Copper (Cu), % 0
0 to 0.050
Iron (Fe), % 70.7 to 77.9
0 to 1.0
Manganese (Mn), % 0 to 2.0
0 to 0.050
Nickel (Ni), % 6.0 to 8.0
0
Nitrogen (N), % 0.070 to 0.2
0
Phosphorus (P), % 0 to 0.045
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

Comparable Variants