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SAE-AISI 1055 Steel vs. Nickel 59

SAE-AISI 1055 steel belongs to the iron alloys classification, while nickel 59 belongs to the nickel 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 SAE-AISI 1055 steel and the bottom bar is nickel 59.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
220
Elongation at Break, % 11 to 14
50
Fatigue Strength, MPa 260 to 390
320
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 72
84
Shear Strength, MPa 440 to 450
560
Tensile Strength: Ultimate (UTS), MPa 730 to 750
780
Tensile Strength: Yield (Proof), MPa 400 to 630
350

Thermal Properties

Latent Heat of Fusion, J/g 250
330
Maximum Temperature: Mechanical, °C 400
990
Melting Completion (Liquidus), °C 1460
1500
Melting Onset (Solidus), °C 1420
1450
Specific Heat Capacity, J/kg-K 470
430
Thermal Conductivity, W/m-K 51
10
Thermal Expansion, µm/m-K 12
17

Otherwise Unclassified Properties

Base Metal Price, % relative 1.8
65
Density, g/cm3 7.8
8.7
Embodied Carbon, kg CO2/kg material 1.4
12
Embodied Energy, MJ/kg 18
160
Embodied Water, L/kg 46
310

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 80 to 85
320
Resilience: Unit (Modulus of Resilience), kJ/m3 440 to 1070
280
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 24
23
Strength to Weight: Axial, points 26
25
Strength to Weight: Bending, points 23
22
Thermal Diffusivity, mm2/s 14
2.7
Thermal Shock Resistance, points 23 to 24
15

Alloy Composition

Aluminum (Al), % 0
0.1 to 0.4
Carbon (C), % 0.5 to 0.6
0 to 0.010
Chromium (Cr), % 0
22 to 24
Cobalt (Co), % 0
0 to 0.3
Copper (Cu), % 0
0 to 0.5
Iron (Fe), % 98.4 to 98.9
0 to 1.5
Manganese (Mn), % 0.6 to 0.9
0 to 0.5
Molybdenum (Mo), % 0
15 to 16.5
Nickel (Ni), % 0
56.2 to 62.9
Phosphorus (P), % 0 to 0.040
0 to 0.015
Silicon (Si), % 0
0 to 0.1
Sulfur (S), % 0 to 0.050
0 to 0.010