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ASTM A182 Grade F10 vs. C34200 Brass

ASTM A182 grade F10 belongs to the iron alloys classification, while C34200 brass belongs to the copper alloys. There are 27 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 ASTM A182 grade F10 and the bottom bar is C34200 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
100
Elongation at Break, % 34
3.0 to 17
Poisson's Ratio 0.29
0.31
Shear Modulus, GPa 74
40
Shear Strength, MPa 420
230 to 360
Tensile Strength: Ultimate (UTS), MPa 630
370 to 650
Tensile Strength: Yield (Proof), MPa 230
150 to 420

Thermal Properties

Latent Heat of Fusion, J/g 290
170
Maximum Temperature: Mechanical, °C 600
120
Melting Completion (Liquidus), °C 1420
910
Melting Onset (Solidus), °C 1370
890
Specific Heat Capacity, J/kg-K 470
380
Thermal Expansion, µm/m-K 13
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 15
26
Electrical Conductivity: Equal Weight (Specific), % IACS 17
29

Otherwise Unclassified Properties

Base Metal Price, % relative 18
24
Density, g/cm3 7.9
8.2
Embodied Carbon, kg CO2/kg material 3.6
2.6
Embodied Energy, MJ/kg 51
45
Embodied Water, L/kg 120
320

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 170
9.0 to 98
Resilience: Unit (Modulus of Resilience), kJ/m3 140
110 to 870
Stiffness to Weight: Axial, points 13
7.1
Stiffness to Weight: Bending, points 24
19
Strength to Weight: Axial, points 22
13 to 22
Strength to Weight: Bending, points 21
14 to 20
Thermal Shock Resistance, points 18
12 to 22

Alloy Composition

Carbon (C), % 0.1 to 0.2
0
Chromium (Cr), % 7.0 to 9.0
0
Copper (Cu), % 0
62 to 65
Iron (Fe), % 66.5 to 72.4
0 to 0.1
Lead (Pb), % 0
1.5 to 2.5
Manganese (Mn), % 0.5 to 0.8
0
Nickel (Ni), % 19 to 22
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 1.0 to 1.4
0
Sulfur (S), % 0 to 0.030
0
Zinc (Zn), % 0
32 to 36.5
Residuals, % 0
0 to 0.4