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Grade CX2M Nickel vs. Nickel 601

Both grade CX2M nickel and nickel 601 are nickel alloys. They have 84% of their average alloy composition in common. 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 grade CX2M nickel and the bottom bar is nickel 601.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 220
200
Elongation at Break, % 45
10 to 38
Fatigue Strength, MPa 260
220 to 380
Poisson's Ratio 0.29
0.28
Shear Modulus, GPa 84
76
Tensile Strength: Ultimate (UTS), MPa 550
660 to 890
Tensile Strength: Yield (Proof), MPa 310
290 to 800

Thermal Properties

Latent Heat of Fusion, J/g 330
320
Maximum Temperature: Mechanical, °C 990
1100
Melting Completion (Liquidus), °C 1500
1410
Melting Onset (Solidus), °C 1450
1360
Specific Heat Capacity, J/kg-K 430
470
Thermal Conductivity, W/m-K 10
11
Thermal Expansion, µm/m-K 12
14

Otherwise Unclassified Properties

Base Metal Price, % relative 65
49
Density, g/cm3 8.7
8.3
Embodied Carbon, kg CO2/kg material 12
8.0
Embodied Energy, MJ/kg 160
110
Embodied Water, L/kg 310
280

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 210
86 to 200
Resilience: Unit (Modulus of Resilience), kJ/m3 220
210 to 1630
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 23
23
Strength to Weight: Axial, points 18
22 to 30
Strength to Weight: Bending, points 17
20 to 25
Thermal Diffusivity, mm2/s 2.7
2.8
Thermal Shock Resistance, points 15
17 to 23

Alloy Composition

Aluminum (Al), % 0
1.0 to 1.7
Carbon (C), % 0 to 0.020
0 to 0.1
Chromium (Cr), % 22 to 24
21 to 25
Copper (Cu), % 0
0 to 1.0
Iron (Fe), % 0 to 1.5
7.7 to 20
Manganese (Mn), % 0 to 1.0
0 to 1.0
Molybdenum (Mo), % 15 to 16.5
0
Nickel (Ni), % 56.4 to 63
58 to 63
Phosphorus (P), % 0 to 0.020
0
Silicon (Si), % 0 to 0.5
0 to 0.5
Sulfur (S), % 0 to 0.020
0 to 0.015