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Hot Rolled SAE-AISI 1010 vs. Hot Worked Nickel 200

Hot rolled SAE-AISI 1010 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 1010 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, % 31
42
Fatigue Strength, MPa 150
120
Poisson's Ratio 0.29
0.31
Shear Modulus, GPa 73
70
Shear Strength, MPa 230
330
Tensile Strength: Ultimate (UTS), MPa 350
480
Tensile Strength: Yield (Proof), MPa 190
150

Thermal Properties

Latent Heat of Fusion, J/g 250
290
Maximum Temperature: Mechanical, °C 400
900
Melting Completion (Liquidus), °C 1470
1460
Melting Onset (Solidus), °C 1430
1440
Specific Heat Capacity, J/kg-K 470
450
Thermal Conductivity, W/m-K 47
69
Thermal Expansion, µm/m-K 12
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 12
18
Electrical Conductivity: Equal Weight (Specific), % IACS 14
18

Otherwise Unclassified Properties

Base Metal Price, % relative 1.8
65
Density, g/cm3 7.9
8.9
Embodied Carbon, kg CO2/kg material 1.4
11
Embodied Energy, MJ/kg 18
150
Embodied Water, L/kg 45
230

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 93
150
Resilience: Unit (Modulus of Resilience), kJ/m3 100
58
Stiffness to Weight: Axial, points 13
11
Stiffness to Weight: Bending, points 24
21
Strength to Weight: Axial, points 12
15
Strength to Weight: Bending, points 14
15
Thermal Diffusivity, mm2/s 13
17
Thermal Shock Resistance, points 11
14

Alloy Composition

Carbon (C), % 0.080 to 0.13
0 to 0.15
Copper (Cu), % 0
0 to 0.25
Iron (Fe), % 99.18 to 99.62
0 to 0.4
Manganese (Mn), % 0.3 to 0.6
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