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Annealed ASTM F15 vs. Annealed SAE-AISI M1

Both annealed ASTM F15 and annealed SAE-AISI M1 are iron alloys. Both are furnished in the annealed condition. They have 54% of their average alloy composition in common. There are 22 material properties with values for both materials. Properties with values for just one material (10, in this case) are not shown.

For each property being compared, the top bar is annealed ASTM F15 and the bottom bar is annealed SAE-AISI M1.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 160
220
Elastic (Young's, Tensile) Modulus, GPa 190
200
Poisson's Ratio 0.3
0.29
Shear Modulus, GPa 73
77
Tensile Strength: Ultimate (UTS), MPa 520
730

Thermal Properties

Latent Heat of Fusion, J/g 270
270
Melting Completion (Liquidus), °C 1410
1560
Melting Onset (Solidus), °C 1450
1510
Specific Heat Capacity, J/kg-K 460
450
Thermal Conductivity, W/m-K 17
29
Thermal Expansion, µm/m-K 6.0
12

Otherwise Unclassified Properties

Base Metal Price, % relative 49
18
Density, g/cm3 8.3
8.1
Embodied Carbon, kg CO2/kg material 5.2
7.0
Embodied Energy, MJ/kg 71
99
Embodied Water, L/kg 190
98

Common Calculations

Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 23
24
Strength to Weight: Axial, points 17
25
Strength to Weight: Bending, points 17
22
Thermal Diffusivity, mm2/s 4.5
8.0
Thermal Shock Resistance, points 32
23

Alloy Composition

Aluminum (Al), % 0 to 0.1
0
Carbon (C), % 0 to 0.040
0.78 to 0.88
Chromium (Cr), % 0 to 0.2
3.5 to 4.0
Cobalt (Co), % 16 to 18
0
Copper (Cu), % 0 to 0.2
0 to 0.25
Iron (Fe), % 50.3 to 56
81 to 84.8
Magnesium (Mg), % 0 to 0.1
0
Manganese (Mn), % 0 to 0.5
0.15 to 0.4
Molybdenum (Mo), % 0 to 0.2
8.2 to 9.2
Nickel (Ni), % 28 to 30
0 to 0.3
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 0.2
0.2 to 0.5
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.1
0
Tungsten (W), % 0
1.4 to 2.1
Vanadium (V), % 0
1.0 to 1.4
Zirconium (Zr), % 0 to 0.1
0