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C36200 Brass vs. ASTM A182 Grade F10

C36200 brass belongs to the copper alloys classification, while ASTM A182 grade F10 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 C36200 brass and the bottom bar is ASTM A182 grade F10.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 100
190
Elongation at Break, % 20 to 53
34
Poisson's Ratio 0.31
0.29
Shear Modulus, GPa 39
74
Shear Strength, MPa 210 to 240
420
Tensile Strength: Ultimate (UTS), MPa 340 to 420
630
Tensile Strength: Yield (Proof), MPa 130 to 360
230

Thermal Properties

Latent Heat of Fusion, J/g 170
290
Maximum Temperature: Mechanical, °C 120
600
Melting Completion (Liquidus), °C 900
1420
Melting Onset (Solidus), °C 890
1370
Specific Heat Capacity, J/kg-K 380
470
Thermal Expansion, µm/m-K 21
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 26
15
Electrical Conductivity: Equal Weight (Specific), % IACS 28
17

Otherwise Unclassified Properties

Base Metal Price, % relative 23
18
Density, g/cm3 8.2
7.9
Embodied Carbon, kg CO2/kg material 2.6
3.6
Embodied Energy, MJ/kg 45
51
Embodied Water, L/kg 320
120

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 74 to 140
170
Resilience: Unit (Modulus of Resilience), kJ/m3 89 to 630
140
Stiffness to Weight: Axial, points 6.9
13
Stiffness to Weight: Bending, points 19
24
Strength to Weight: Axial, points 11 to 14
22
Strength to Weight: Bending, points 13 to 15
21
Thermal Shock Resistance, points 11 to 14
18

Alloy Composition

Carbon (C), % 0
0.1 to 0.2
Chromium (Cr), % 0
7.0 to 9.0
Copper (Cu), % 60 to 63
0
Iron (Fe), % 0 to 0.15
66.5 to 72.4
Lead (Pb), % 3.5 to 4.5
0
Manganese (Mn), % 0
0.5 to 0.8
Nickel (Ni), % 0
19 to 22
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0
1.0 to 1.4
Sulfur (S), % 0
0 to 0.030
Zinc (Zn), % 32.4 to 36.5
0