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C66900 Brass vs. SAE-AISI 1026 Steel

C66900 brass belongs to the copper alloys classification, while SAE-AISI 1026 steel belongs to the iron 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 C66900 brass and the bottom bar is SAE-AISI 1026 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
190
Elongation at Break, % 1.1 to 26
17 to 27
Poisson's Ratio 0.32
0.29
Shear Modulus, GPa 45
73
Shear Strength, MPa 290 to 440
320 to 340
Tensile Strength: Ultimate (UTS), MPa 460 to 770
500 to 550
Tensile Strength: Yield (Proof), MPa 330 to 760
270 to 470

Thermal Properties

Latent Heat of Fusion, J/g 190
250
Maximum Temperature: Mechanical, °C 150
400
Melting Completion (Liquidus), °C 860
1460
Melting Onset (Solidus), °C 850
1420
Specific Heat Capacity, J/kg-K 400
470
Thermal Expansion, µm/m-K 20
12

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 3.4
7.0
Electrical Conductivity: Equal Weight (Specific), % IACS 3.8
8.0

Otherwise Unclassified Properties

Base Metal Price, % relative 23
1.8
Density, g/cm3 8.2
7.9
Embodied Carbon, kg CO2/kg material 2.8
1.4
Embodied Energy, MJ/kg 46
18
Embodied Water, L/kg 310
46

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.6 to 200
89 to 110
Resilience: Unit (Modulus of Resilience), kJ/m3 460 to 2450
200 to 580
Stiffness to Weight: Axial, points 8.1
13
Stiffness to Weight: Bending, points 20
24
Strength to Weight: Axial, points 15 to 26
18 to 20
Strength to Weight: Bending, points 16 to 23
18 to 19
Thermal Shock Resistance, points 14 to 23
16 to 18

Alloy Composition

Carbon (C), % 0
0.22 to 0.28
Copper (Cu), % 62.5 to 64.5
0
Iron (Fe), % 0 to 0.25
98.7 to 99.18
Lead (Pb), % 0 to 0.050
0
Manganese (Mn), % 11.5 to 12.5
0.6 to 0.9
Phosphorus (P), % 0
0 to 0.040
Sulfur (S), % 0
0 to 0.050
Zinc (Zn), % 22.5 to 26
0
Residuals, % 0 to 0.2
0