MakeItFrom.com
Menu (ESC)

EN 1.4005 Stainless Steel vs. 712.0 Aluminum

EN 1.4005 stainless steel belongs to the iron alloys classification, while 712.0 aluminum belongs to the aluminum alloys. There are 30 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 EN 1.4005 stainless steel and the bottom bar is 712.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
70
Elongation at Break, % 13 to 21
4.5 to 4.7
Fatigue Strength, MPa 240 to 290
140 to 180
Poisson's Ratio 0.28
0.32
Shear Modulus, GPa 76
27
Shear Strength, MPa 390 to 450
180
Tensile Strength: Ultimate (UTS), MPa 630 to 750
250 to 260
Tensile Strength: Yield (Proof), MPa 370 to 500
180 to 200

Thermal Properties

Latent Heat of Fusion, J/g 270
380
Maximum Temperature: Mechanical, °C 760
190
Melting Completion (Liquidus), °C 1440
640
Melting Onset (Solidus), °C 1400
610
Specific Heat Capacity, J/kg-K 480
870
Thermal Conductivity, W/m-K 30
160
Thermal Expansion, µm/m-K 10
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.9
40
Electrical Conductivity: Equal Weight (Specific), % IACS 3.3
120

Otherwise Unclassified Properties

Base Metal Price, % relative 7.0
9.5
Density, g/cm3 7.7
3.0
Embodied Carbon, kg CO2/kg material 2.0
8.0
Embodied Energy, MJ/kg 28
150
Embodied Water, L/kg 100
1140

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 90 to 110
11
Resilience: Unit (Modulus of Resilience), kJ/m3 350 to 650
240 to 270
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
46
Strength to Weight: Axial, points 23 to 27
24 to 25
Strength to Weight: Bending, points 21 to 24
30 to 31
Thermal Diffusivity, mm2/s 8.1
62
Thermal Shock Resistance, points 23 to 27
11

Alloy Composition

Aluminum (Al), % 0
90.7 to 94
Carbon (C), % 0.060 to 0.15
0
Chromium (Cr), % 12 to 14
0.4 to 0.6
Copper (Cu), % 0
0 to 0.25
Iron (Fe), % 82.4 to 87.8
0 to 0.5
Magnesium (Mg), % 0
0.5 to 0.65
Manganese (Mn), % 0 to 1.5
0 to 0.1
Molybdenum (Mo), % 0 to 0.6
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0 to 1.0
0 to 0.3
Sulfur (S), % 0.15 to 0.35
0
Titanium (Ti), % 0
0.15 to 0.25
Zinc (Zn), % 0
5.0 to 6.5
Residuals, % 0
0 to 0.2