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C46200 Brass vs. ASTM A182 Grade F6b

C46200 brass belongs to the copper alloys classification, while ASTM A182 grade F6b belongs to the iron alloys. There are 27 material properties with values for both materials. Properties with values for just one material (7, in this case) are not shown.

For each property being compared, the top bar is C46200 brass and the bottom bar is ASTM A182 grade F6b.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 100
190
Elongation at Break, % 17 to 34
18
Poisson's Ratio 0.31
0.28
Shear Modulus, GPa 40
76
Shear Strength, MPa 240 to 290
530
Tensile Strength: Ultimate (UTS), MPa 370 to 480
850
Tensile Strength: Yield (Proof), MPa 120 to 290
710

Thermal Properties

Latent Heat of Fusion, J/g 170
280
Maximum Temperature: Mechanical, °C 120
750
Melting Completion (Liquidus), °C 840
1450
Melting Onset (Solidus), °C 800
1400
Specific Heat Capacity, J/kg-K 380
480
Thermal Conductivity, W/m-K 110
25
Thermal Expansion, µm/m-K 20
10

Otherwise Unclassified Properties

Base Metal Price, % relative 24
8.0
Density, g/cm3 8.1
7.8
Embodied Carbon, kg CO2/kg material 2.7
2.2
Embodied Energy, MJ/kg 46
30
Embodied Water, L/kg 330
100

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 69 to 100
140
Resilience: Unit (Modulus of Resilience), kJ/m3 72 to 400
1280
Stiffness to Weight: Axial, points 7.2
14
Stiffness to Weight: Bending, points 19
25
Strength to Weight: Axial, points 13 to 16
30
Strength to Weight: Bending, points 14 to 17
26
Thermal Diffusivity, mm2/s 35
6.7
Thermal Shock Resistance, points 12 to 16
31

Alloy Composition

Carbon (C), % 0
0 to 0.15
Chromium (Cr), % 0
11.5 to 13.5
Copper (Cu), % 62 to 65
0 to 0.5
Iron (Fe), % 0 to 0.1
81.2 to 87.1
Lead (Pb), % 0 to 0.2
0
Manganese (Mn), % 0
0 to 1.0
Molybdenum (Mo), % 0
0.4 to 0.6
Nickel (Ni), % 0
1.0 to 2.0
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0
0 to 1.0
Sulfur (S), % 0
0 to 0.020
Tin (Sn), % 0.5 to 1.0
0
Zinc (Zn), % 33.3 to 37.5
0
Residuals, % 0 to 0.4
0