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Hot Rolled SAE-AISI 1524 vs. Hot Worked Nickel 200

Hot rolled SAE-AISI 1524 belongs to the iron alloys classification, while hot worked nickel 200 belongs to the nickel alloys. There are 30 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 hot rolled SAE-AISI 1524 and the bottom bar is hot worked nickel 200.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
180
Elongation at Break, % 22
42
Fatigue Strength, MPa 230
120
Poisson's Ratio 0.29
0.31
Shear Modulus, GPa 73
70
Shear Strength, MPa 360
330
Tensile Strength: Ultimate (UTS), MPa 570
480
Tensile Strength: Yield (Proof), MPa 320
150

Thermal Properties

Latent Heat of Fusion, J/g 250
290
Maximum Temperature: Mechanical, °C 400
900
Melting Completion (Liquidus), °C 1460
1460
Melting Onset (Solidus), °C 1420
1440
Specific Heat Capacity, J/kg-K 470
450
Thermal Conductivity, W/m-K 52
69
Thermal Expansion, µm/m-K 12
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 8.3
18
Electrical Conductivity: Equal Weight (Specific), % IACS 9.5
18

Otherwise Unclassified Properties

Base Metal Price, % relative 1.9
65
Density, g/cm3 7.8
8.9
Embodied Carbon, kg CO2/kg material 1.4
11
Embodied Energy, MJ/kg 19
150
Embodied Water, L/kg 48
230

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110
150
Resilience: Unit (Modulus of Resilience), kJ/m3 270
58
Stiffness to Weight: Axial, points 13
11
Stiffness to Weight: Bending, points 24
21
Strength to Weight: Axial, points 20
15
Strength to Weight: Bending, points 19
15
Thermal Diffusivity, mm2/s 14
17
Thermal Shock Resistance, points 18
14

Alloy Composition

Carbon (C), % 0.19 to 0.25
0 to 0.15
Copper (Cu), % 0
0 to 0.25
Iron (Fe), % 98 to 98.5
0 to 0.4
Manganese (Mn), % 1.4 to 1.7
0 to 0.35
Nickel (Ni), % 0
99 to 100
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0
0 to 0.35
Sulfur (S), % 0 to 0.050
0 to 0.010