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Grade M35-1 Nickel vs. Nickel 890

Both grade M35-1 nickel and nickel 890 are nickel alloys. They have 46% of their average alloy composition in common. There are 25 material properties with values for both materials. Properties with values for just one material (5, in this case) are not shown.

For each property being compared, the top bar is grade M35-1 nickel and the bottom bar is nickel 890.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 160
200
Elongation at Break, % 28
39
Fatigue Strength, MPa 130
180
Poisson's Ratio 0.32
0.28
Shear Modulus, GPa 62
78
Tensile Strength: Ultimate (UTS), MPa 500
590
Tensile Strength: Yield (Proof), MPa 190
230

Thermal Properties

Latent Heat of Fusion, J/g 280
330
Maximum Temperature: Mechanical, °C 900
1000
Melting Completion (Liquidus), °C 1280
1390
Melting Onset (Solidus), °C 1240
1340
Specific Heat Capacity, J/kg-K 430
480
Thermal Expansion, µm/m-K 13
14

Otherwise Unclassified Properties

Base Metal Price, % relative 55
47
Density, g/cm3 8.8
8.1
Embodied Carbon, kg CO2/kg material 8.2
8.2
Embodied Energy, MJ/kg 120
120
Embodied Water, L/kg 250
250

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110
180
Resilience: Unit (Modulus of Resilience), kJ/m3 120
140
Stiffness to Weight: Axial, points 10
14
Stiffness to Weight: Bending, points 21
24
Strength to Weight: Axial, points 16
20
Strength to Weight: Bending, points 16
19
Thermal Shock Resistance, points 17
15

Alloy Composition

Aluminum (Al), % 0
0.050 to 0.6
Carbon (C), % 0 to 0.35
0.060 to 0.14
Chromium (Cr), % 0
23.5 to 28.5
Copper (Cu), % 26 to 33
0 to 0.75
Iron (Fe), % 0 to 3.5
17.3 to 33.9
Manganese (Mn), % 0 to 1.5
0 to 1.5
Molybdenum (Mo), % 0
1.0 to 2.0
Nickel (Ni), % 59.8 to 74
40 to 45
Niobium (Nb), % 0 to 0.5
0.2 to 1.0
Phosphorus (P), % 0 to 0.030
0
Silicon (Si), % 0 to 1.3
1.0 to 2.0
Sulfur (S), % 0 to 0.030
0 to 0.015
Tantalum (Ta), % 0
0.1 to 0.6
Titanium (Ti), % 0
0.15 to 0.6