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C85200 Brass vs. SAE-AISI M1 Steel

C85200 brass belongs to the copper alloys classification, while SAE-AISI M1 steel belongs to the iron 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 C85200 brass and the bottom bar is SAE-AISI M1 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
200
Poisson's Ratio 0.32
0.29
Shear Modulus, GPa 40
77
Tensile Strength: Ultimate (UTS), MPa 270
730 to 2140

Thermal Properties

Latent Heat of Fusion, J/g 180
270
Melting Completion (Liquidus), °C 940
1560
Melting Onset (Solidus), °C 930
1510
Specific Heat Capacity, J/kg-K 380
450
Thermal Conductivity, W/m-K 84
29
Thermal Expansion, µm/m-K 20
12

Otherwise Unclassified Properties

Base Metal Price, % relative 26
18
Density, g/cm3 8.4
8.1
Embodied Carbon, kg CO2/kg material 2.8
7.0
Embodied Energy, MJ/kg 46
99
Embodied Water, L/kg 330
98

Common Calculations

Stiffness to Weight: Axial, points 7.0
14
Stiffness to Weight: Bending, points 19
24
Strength to Weight: Axial, points 8.9
25 to 73
Strength to Weight: Bending, points 11
22 to 45
Thermal Diffusivity, mm2/s 27
8.0
Thermal Shock Resistance, points 9.3
23 to 66

Alloy Composition

Aluminum (Al), % 0 to 0.0050
0
Antimony (Sb), % 0 to 0.2
0
Carbon (C), % 0
0.78 to 0.88
Chromium (Cr), % 0
3.5 to 4.0
Copper (Cu), % 70 to 74
0 to 0.25
Iron (Fe), % 0 to 0.6
81 to 84.8
Lead (Pb), % 1.5 to 3.8
0
Manganese (Mn), % 0
0.15 to 0.4
Molybdenum (Mo), % 0
8.2 to 9.2
Nickel (Ni), % 0 to 1.0
0 to 0.3
Phosphorus (P), % 0 to 0.020
0 to 0.030
Silicon (Si), % 0 to 0.050
0.2 to 0.5
Sulfur (S), % 0 to 0.050
0 to 0.030
Tin (Sn), % 0.7 to 2.0
0
Tungsten (W), % 0
1.4 to 2.1
Vanadium (V), % 0
1.0 to 1.4
Zinc (Zn), % 20 to 27
0
Residuals, % 0 to 0.9
0