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Hot Rolled SAE-AISI 1552 vs. Hot Worked Monel 400

Hot rolled SAE-AISI 1552 belongs to the iron alloys classification, while hot worked Monel 400 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 1552 and the bottom bar is hot worked Monel 400.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
160
Elongation at Break, % 14
37
Fatigue Strength, MPa 290
290
Poisson's Ratio 0.29
0.32
Shear Modulus, GPa 72
62
Shear Strength, MPa 510
400
Tensile Strength: Ultimate (UTS), MPa 840
600
Tensile Strength: Yield (Proof), MPa 460
260

Thermal Properties

Latent Heat of Fusion, J/g 250
270
Maximum Temperature: Mechanical, °C 400
1000
Melting Completion (Liquidus), °C 1460
1350
Melting Onset (Solidus), °C 1420
1300
Specific Heat Capacity, J/kg-K 470
430
Thermal Conductivity, W/m-K 51
23
Thermal Expansion, µm/m-K 11
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 11
3.3
Electrical Conductivity: Equal Weight (Specific), % IACS 12
3.4

Otherwise Unclassified Properties

Base Metal Price, % relative 1.8
50
Density, g/cm3 7.8
8.9
Embodied Carbon, kg CO2/kg material 1.4
7.9
Embodied Energy, MJ/kg 19
110
Embodied Water, L/kg 47
250

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 98
180
Resilience: Unit (Modulus of Resilience), kJ/m3 560
210
Stiffness to Weight: Axial, points 13
10
Stiffness to Weight: Bending, points 24
21
Strength to Weight: Axial, points 30
19
Strength to Weight: Bending, points 25
18
Thermal Diffusivity, mm2/s 14
6.1
Thermal Shock Resistance, points 29
19

Alloy Composition

Carbon (C), % 0.47 to 0.55
0 to 0.3
Copper (Cu), % 0
28 to 34
Iron (Fe), % 97.9 to 98.3
0 to 2.5
Manganese (Mn), % 1.2 to 1.5
0 to 2.0
Nickel (Ni), % 0
63 to 72
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0
0 to 0.5
Sulfur (S), % 0 to 0.050
0 to 0.024