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ASTM A182 Grade F10 vs. C27200 Brass

ASTM A182 grade F10 belongs to the iron alloys classification, while C27200 brass belongs to the copper 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 ASTM A182 grade F10 and the bottom bar is C27200 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
110
Elongation at Break, % 34
10 to 50
Poisson's Ratio 0.29
0.31
Shear Modulus, GPa 74
40
Shear Strength, MPa 420
230 to 320
Tensile Strength: Ultimate (UTS), MPa 630
370 to 590
Tensile Strength: Yield (Proof), MPa 230
150 to 410

Thermal Properties

Latent Heat of Fusion, J/g 290
170
Maximum Temperature: Mechanical, °C 600
130
Melting Completion (Liquidus), °C 1420
920
Melting Onset (Solidus), °C 1370
870
Specific Heat Capacity, J/kg-K 470
390
Thermal Expansion, µm/m-K 13
20

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 15
28
Electrical Conductivity: Equal Weight (Specific), % IACS 17
31

Otherwise Unclassified Properties

Base Metal Price, % relative 18
24
Density, g/cm3 7.9
8.1
Embodied Carbon, kg CO2/kg material 3.6
2.7
Embodied Energy, MJ/kg 51
45
Embodied Water, L/kg 120
320

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 170
30 to 270
Resilience: Unit (Modulus of Resilience), kJ/m3 140
110 to 810
Stiffness to Weight: Axial, points 13
7.2
Stiffness to Weight: Bending, points 24
19
Strength to Weight: Axial, points 22
13 to 20
Strength to Weight: Bending, points 21
14 to 19
Thermal Shock Resistance, points 18
12 to 20

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 0.070
Lead (Pb), % 0
0 to 0.070
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
34.6 to 38
Residuals, % 0
0 to 0.3