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Nickel 80A vs. C68300 Brass

Nickel 80A belongs to the nickel alloys classification, while C68300 brass belongs to the copper 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 nickel 80A and the bottom bar is C68300 brass.

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition

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