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Nickel 59 vs. SAE-AISI 1008 Steel

Nickel 59 belongs to the nickel alloys classification, while SAE-AISI 1008 steel belongs to the iron alloys. There are 28 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 59 and the bottom bar is SAE-AISI 1008 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 220
190
Elongation at Break, % 50
22 to 33
Fatigue Strength, MPa 320
150 to 220
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 84
73
Shear Strength, MPa 560
220 to 230
Tensile Strength: Ultimate (UTS), MPa 780
330 to 370
Tensile Strength: Yield (Proof), MPa 350
190 to 310

Thermal Properties

Latent Heat of Fusion, J/g 330
250
Maximum Temperature: Mechanical, °C 990
400
Melting Completion (Liquidus), °C 1500
1470
Melting Onset (Solidus), °C 1450
1430
Specific Heat Capacity, J/kg-K 430
470
Thermal Conductivity, W/m-K 10
62
Thermal Expansion, µm/m-K 17
12

Otherwise Unclassified Properties

Base Metal Price, % relative 65
1.8
Density, g/cm3 8.7
7.9
Embodied Carbon, kg CO2/kg material 12
1.4
Embodied Energy, MJ/kg 160
18
Embodied Water, L/kg 310
45

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 320
78 to 91
Resilience: Unit (Modulus of Resilience), kJ/m3 280
92 to 260
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 23
24
Strength to Weight: Axial, points 25
12 to 13
Strength to Weight: Bending, points 22
13 to 15
Thermal Diffusivity, mm2/s 2.7
17
Thermal Shock Resistance, points 15
10 to 12

Alloy Composition

Aluminum (Al), % 0.1 to 0.4
0
Carbon (C), % 0 to 0.010
0 to 0.1
Chromium (Cr), % 22 to 24
0
Cobalt (Co), % 0 to 0.3
0
Copper (Cu), % 0 to 0.5
0
Iron (Fe), % 0 to 1.5
99.31 to 99.7
Manganese (Mn), % 0 to 0.5
0.3 to 0.5
Molybdenum (Mo), % 15 to 16.5
0
Nickel (Ni), % 56.2 to 62.9
0
Phosphorus (P), % 0 to 0.015
0 to 0.040
Silicon (Si), % 0 to 0.1
0
Sulfur (S), % 0 to 0.010
0 to 0.050