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H01 C26200 Brass vs. H01 C36200 Brass

Both H01 C26200 brass and H01 C36200 brass are copper alloys. Both are furnished in the H01 (quarter hard) temper. They have a moderately high 93% of their average alloy composition in common. There are 30 material properties with values for both materials. Properties with values for just one material (1, in this case) are not shown.

For each property being compared, the top bar is H01 C26200 brass and the bottom bar is H01 C36200 brass.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 110
100
Elongation at Break, % 32
20
Poisson's Ratio 0.31
0.31
Rockwell B Hardness 55
62
Shear Modulus, GPa 41
39
Shear Strength, MPa 250
230
Tensile Strength: Ultimate (UTS), MPa 430
390
Tensile Strength: Yield (Proof), MPa 300
340

Thermal Properties

Latent Heat of Fusion, J/g 180
170
Maximum Temperature: Mechanical, °C 140
120
Melting Completion (Liquidus), °C 950
900
Melting Onset (Solidus), °C 920
890
Specific Heat Capacity, J/kg-K 390
380
Thermal Conductivity, W/m-K 120
120
Thermal Expansion, µm/m-K 20
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 28
26
Electrical Conductivity: Equal Weight (Specific), % IACS 31
28

Otherwise Unclassified Properties

Base Metal Price, % relative 25
23
Density, g/cm3 8.2
8.2
Embodied Carbon, kg CO2/kg material 2.7
2.6
Embodied Energy, MJ/kg 45
45
Embodied Water, L/kg 320
320

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 120
74
Resilience: Unit (Modulus of Resilience), kJ/m3 420
560
Stiffness to Weight: Axial, points 7.2
6.9
Stiffness to Weight: Bending, points 19
19
Strength to Weight: Axial, points 14
13
Strength to Weight: Bending, points 15
14
Thermal Diffusivity, mm2/s 38
37
Thermal Shock Resistance, points 14
13

Alloy Composition

Copper (Cu), % 67 to 70
60 to 63
Iron (Fe), % 0 to 0.050
0 to 0.15
Lead (Pb), % 0 to 0.070
3.5 to 4.5
Zinc (Zn), % 29.6 to 33
32.4 to 36.5
Residuals, % 0 to 0.3
0