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SAE-AISI T8 Steel vs. C85200 Brass

SAE-AISI T8 steel belongs to the iron alloys classification, while C85200 brass belongs to the copper alloys. There are 21 material properties with values for both materials. Properties with values for just one material (8, in this case) are not shown.

For each property being compared, the top bar is SAE-AISI T8 steel and the bottom bar is C85200 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
110
Poisson's Ratio 0.29
0.32
Shear Modulus, GPa 78
40
Tensile Strength: Ultimate (UTS), MPa 780 to 2140
270

Thermal Properties

Latent Heat of Fusion, J/g 250
180
Melting Completion (Liquidus), °C 1730
940
Melting Onset (Solidus), °C 1670
930
Specific Heat Capacity, J/kg-K 420
380
Thermal Conductivity, W/m-K 18
84
Thermal Expansion, µm/m-K 12
20

Otherwise Unclassified Properties

Base Metal Price, % relative 45
26
Density, g/cm3 9.0
8.4
Embodied Carbon, kg CO2/kg material 10
2.8
Embodied Energy, MJ/kg 160
46
Embodied Water, L/kg 120
330

Common Calculations

Stiffness to Weight: Axial, points 12
7.0
Stiffness to Weight: Bending, points 22
19
Strength to Weight: Axial, points 24 to 66
8.9
Strength to Weight: Bending, points 21 to 41
11
Thermal Diffusivity, mm2/s 4.8
27
Thermal Shock Resistance, points 24 to 66
9.3

Alloy Composition


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Aluminum (Al), % 0
0 to 0.0050
Antimony (Sb), % 0
0 to 0.2
Carbon (C), % 0.75 to 0.85
0
Chromium (Cr), % 3.8 to 4.5
0
Cobalt (Co), % 4.3 to 5.8
0
Copper (Cu), % 0 to 0.25
70 to 74
Iron (Fe), % 69.3 to 75.4
0 to 0.6
Lead (Pb), % 0
1.5 to 3.8
Manganese (Mn), % 0.2 to 0.4
0
Molybdenum (Mo), % 0.4 to 1.0
0
Nickel (Ni), % 0 to 0.3
0 to 1.0
Phosphorus (P), % 0 to 0.030
0 to 0.020
Silicon (Si), % 0.2 to 0.4
0 to 0.050
Sulfur (S), % 0 to 0.030
0 to 0.050
Tin (Sn), % 0
0.7 to 2.0
Tungsten (W), % 13.3 to 14.8
0
Vanadium (V), % 1.8 to 2.4
0
Zinc (Zn), % 0
20 to 27
Residuals, % 0
0 to 0.9