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C68300 Brass vs. Nickel 80A

C68300 brass belongs to the copper alloys classification, while nickel 80A belongs to the nickel alloys. There are 27 material properties with values for both materials. Properties with values for just one material (4, in this case) are not shown.

For each property being compared, the top bar is C68300 brass and the bottom bar is nickel 80A.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 100
190
Elongation at Break, % 15
22
Poisson's Ratio 0.31
0.29
Shear Modulus, GPa 40
74
Shear Strength, MPa 260
660
Tensile Strength: Ultimate (UTS), MPa 430
1040
Tensile Strength: Yield (Proof), MPa 260
710

Thermal Properties

Latent Heat of Fusion, J/g 180
320
Maximum Temperature: Mechanical, °C 120
980
Melting Completion (Liquidus), °C 900
1360
Melting Onset (Solidus), °C 890
1310
Specific Heat Capacity, J/kg-K 390
470
Thermal Conductivity, W/m-K 120
11
Thermal Expansion, µm/m-K 20
13

Otherwise Unclassified Properties

Base Metal Price, % relative 23
55
Density, g/cm3 8.0
8.3
Embodied Carbon, kg CO2/kg material 2.8
9.8
Embodied Energy, MJ/kg 46
140
Embodied Water, L/kg 340
280

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 56
210
Resilience: Unit (Modulus of Resilience), kJ/m3 330
1300
Stiffness to Weight: Axial, points 7.3
13
Stiffness to Weight: Bending, points 20
23
Strength to Weight: Axial, points 15
35
Strength to Weight: Bending, points 16
27
Thermal Diffusivity, mm2/s 38
2.9
Thermal Shock Resistance, points 14
31

Alloy Composition

Aluminum (Al), % 0
0.5 to 1.8
Antimony (Sb), % 0.3 to 1.0
0
Cadmium (Cd), % 0 to 0.010
0
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0
18 to 21
Copper (Cu), % 59 to 63
0
Iron (Fe), % 0
0 to 3.0
Lead (Pb), % 0 to 0.090
0
Manganese (Mn), % 0
0 to 1.0
Nickel (Ni), % 0
69.4 to 79.7
Silicon (Si), % 0.3 to 1.0
0 to 1.0
Sulfur (S), % 0
0 to 0.015
Tin (Sn), % 0.050 to 0.2
0
Titanium (Ti), % 0
1.8 to 2.7
Zinc (Zn), % 34.2 to 40.4
0
Residuals, % 0 to 0.5
0