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ASTM A182 Grade F10 vs. C37100 Brass

ASTM A182 grade F10 belongs to the iron alloys classification, while C37100 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 C37100 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
100
Elongation at Break, % 34
8.0 to 40
Poisson's Ratio 0.29
0.31
Shear Modulus, GPa 74
40
Shear Strength, MPa 420
260 to 300
Tensile Strength: Ultimate (UTS), MPa 630
370 to 520
Tensile Strength: Yield (Proof), MPa 230
150 to 390

Thermal Properties

Latent Heat of Fusion, J/g 290
170
Maximum Temperature: Mechanical, °C 600
120
Melting Completion (Liquidus), °C 1420
900
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
27
Electrical Conductivity: Equal Weight (Specific), % IACS 17
30

Otherwise Unclassified Properties

Base Metal Price, % relative 18
23
Density, g/cm3 7.9
8.0
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
38 to 120
Resilience: Unit (Modulus of Resilience), kJ/m3 140
110 to 750
Stiffness to Weight: Axial, points 13
7.2
Stiffness to Weight: Bending, points 24
20
Strength to Weight: Axial, points 22
13 to 18
Strength to Weight: Bending, points 21
14 to 18
Thermal Shock Resistance, points 18
12 to 17

Alloy Composition


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Carbon (C), % 0.1 to 0.2
0
Chromium (Cr), % 7.0 to 9.0
0
Copper (Cu), % 0
58 to 62
Iron (Fe), % 66.5 to 72.4
0 to 0.15
Lead (Pb), % 0
0.6 to 1.2
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
36.3 to 41.4
Residuals, % 0
0 to 0.4