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Hot Rolled SAE-AISI 1552 vs. Hot Worked Nickel 201

Hot rolled SAE-AISI 1552 belongs to the iron alloys classification, while hot worked nickel 201 belongs to the nickel alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, in this case) are not shown.

For each property being compared, the top bar is hot rolled SAE-AISI 1552 and the bottom bar is hot worked nickel 201.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
180
Elongation at Break, % 14
45
Fatigue Strength, MPa 290
68
Poisson's Ratio 0.29
0.31
Shear Modulus, GPa 72
70
Shear Strength, MPa 510
270
Tensile Strength: Ultimate (UTS), MPa 840
390
Tensile Strength: Yield (Proof), MPa 460
80

Thermal Properties

Latent Heat of Fusion, J/g 250
290
Maximum Temperature: Mechanical, °C 400
900
Melting Completion (Liquidus), °C 1460
1450
Melting Onset (Solidus), °C 1420
1440
Specific Heat Capacity, J/kg-K 470
440
Thermal Conductivity, W/m-K 51
78
Thermal Expansion, µm/m-K 11
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 11
19
Electrical Conductivity: Equal Weight (Specific), % IACS 12
19

Otherwise Unclassified Properties

Base Metal Price, % relative 1.8
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 47
230

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 98
130
Resilience: Unit (Modulus of Resilience), kJ/m3 560
17
Stiffness to Weight: Axial, points 13
11
Stiffness to Weight: Bending, points 24
21
Strength to Weight: Axial, points 30
12
Strength to Weight: Bending, points 25
13
Thermal Diffusivity, mm2/s 14
20
Thermal Shock Resistance, points 29
11

Alloy Composition

Carbon (C), % 0.47 to 0.55
0 to 0.020
Copper (Cu), % 0
0 to 0.25
Iron (Fe), % 97.9 to 98.3
0 to 0.4
Manganese (Mn), % 1.2 to 1.5
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