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ASTM A182 Grade F10 vs. C33200 Brass

ASTM A182 grade F10 belongs to the iron alloys classification, while C33200 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 C33200 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
100
Elongation at Break, % 34
7.0 to 60
Poisson's Ratio 0.29
0.31
Shear Modulus, GPa 74
40
Shear Strength, MPa 420
240 to 300
Tensile Strength: Ultimate (UTS), MPa 630
320 to 520
Tensile Strength: Yield (Proof), MPa 230
110 to 450

Thermal Properties

Latent Heat of Fusion, J/g 290
170
Maximum Temperature: Mechanical, °C 600
130
Melting Completion (Liquidus), °C 1420
930
Melting Onset (Solidus), °C 1370
900
Specific Heat Capacity, J/kg-K 470
380
Thermal Expansion, µm/m-K 13
20

Electrical Properties

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

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
44
Embodied Water, L/kg 120
320

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 170
35 to 150
Resilience: Unit (Modulus of Resilience), kJ/m3 140
60 to 960
Stiffness to Weight: Axial, points 13
7.1
Stiffness to Weight: Bending, points 24
19
Strength to Weight: Axial, points 22
11 to 17
Strength to Weight: Bending, points 21
13 to 17
Thermal Shock Resistance, points 18
11 to 17

Alloy Composition

Carbon (C), % 0.1 to 0.2
0
Chromium (Cr), % 7.0 to 9.0
0
Copper (Cu), % 0
65 to 68
Iron (Fe), % 66.5 to 72.4
0 to 0.070
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
29 to 33.5
Residuals, % 0
0 to 0.4