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Annealed ASTM F15 vs. Annealed SAE-AISI H25

Both annealed ASTM F15 and annealed SAE-AISI H25 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 (9, 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 H25.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 160
210
Elastic (Young's, Tensile) Modulus, GPa 190
200
Poisson's Ratio 0.3
0.29
Shear Modulus, GPa 73
79
Tensile Strength: Ultimate (UTS), MPa 520
710

Thermal Properties

Latent Heat of Fusion, J/g 270
250
Melting Completion (Liquidus), °C 1410
1750
Melting Onset (Solidus), °C 1450
1700
Specific Heat Capacity, J/kg-K 460
420
Thermal Conductivity, W/m-K 17
26
Thermal Expansion, µm/m-K 6.0
12

Otherwise Unclassified Properties

Base Metal Price, % relative 49
38
Density, g/cm3 8.3
9.1
Embodied Carbon, kg CO2/kg material 5.2
6.2
Embodied Energy, MJ/kg 71
93
Embodied Water, L/kg 190
83

Common Calculations

Stiffness to Weight: Axial, points 13
12
Stiffness to Weight: Bending, points 23
22
Strength to Weight: Axial, points 17
22
Strength to Weight: Bending, points 17
20
Thermal Diffusivity, mm2/s 4.5
6.7
Thermal Shock Resistance, points 32
22

Alloy Composition

Aluminum (Al), % 0 to 0.1
0
Carbon (C), % 0 to 0.040
0.22 to 0.32
Chromium (Cr), % 0 to 0.2
3.8 to 4.5
Cobalt (Co), % 16 to 18
0
Copper (Cu), % 0 to 0.2
0 to 0.25
Iron (Fe), % 50.3 to 56
77.2 to 81.3
Magnesium (Mg), % 0 to 0.1
0
Manganese (Mn), % 0 to 0.5
0.15 to 0.4
Molybdenum (Mo), % 0 to 0.2
0
Nickel (Ni), % 28 to 30
0 to 0.3
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 0.2
0.15 to 0.4
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.1
0
Tungsten (W), % 0
14 to 16
Vanadium (V), % 0
0.4 to 0.6
Zirconium (Zr), % 0 to 0.1
0