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Annealed SAE-AISI T8 vs. Annealed K93500 Alloy

Both annealed SAE-AISI T8 and annealed K93500 alloy are iron alloys. Both are furnished in the annealed condition. They have 68% of their average alloy composition in common. There are 21 material properties with values for both materials. Properties with values for just one material (5, in this case) are not shown.

For each property being compared, the top bar is annealed SAE-AISI T8 and the bottom bar is annealed K93500 alloy.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 240
160
Elastic (Young's, Tensile) Modulus, GPa 200
190
Poisson's Ratio 0.29
0.3
Rockwell B Hardness 100
73
Shear Modulus, GPa 78
72
Tensile Strength: Ultimate (UTS), MPa 780
490

Thermal Properties

Latent Heat of Fusion, J/g 250
270
Melting Completion (Liquidus), °C 1730
1430
Melting Onset (Solidus), °C 1670
1380
Specific Heat Capacity, J/kg-K 420
460
Thermal Expansion, µm/m-K 12
12

Otherwise Unclassified Properties

Base Metal Price, % relative 45
30
Density, g/cm3 9.0
8.2
Embodied Carbon, kg CO2/kg material 10
4.7
Embodied Energy, MJ/kg 160
65
Embodied Water, L/kg 120
130

Common Calculations

Stiffness to Weight: Axial, points 12
13
Stiffness to Weight: Bending, points 22
23
Strength to Weight: Axial, points 24
17
Strength to Weight: Bending, points 21
17
Thermal Shock Resistance, points 24
15

Alloy Composition

Aluminum (Al), % 0
0 to 0.1
Carbon (C), % 0.75 to 0.85
0 to 0.050
Chromium (Cr), % 3.8 to 4.5
0 to 0.25
Cobalt (Co), % 4.3 to 5.8
5.0
Copper (Cu), % 0 to 0.25
0
Iron (Fe), % 69.3 to 75.4
61.4 to 63
Magnesium (Mg), % 0
0 to 0.1
Manganese (Mn), % 0.2 to 0.4
0 to 0.6
Molybdenum (Mo), % 0.4 to 1.0
0
Nickel (Ni), % 0 to 0.3
32
Phosphorus (P), % 0 to 0.030
0 to 0.015
Silicon (Si), % 0.2 to 0.4
0 to 0.25
Sulfur (S), % 0 to 0.030
0 to 0.015
Titanium (Ti), % 0
0 to 0.1
Tungsten (W), % 13.3 to 14.8
0
Vanadium (V), % 1.8 to 2.4
0
Zirconium (Zr), % 0
0 to 0.1