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Annealed 250 Maraging Steel vs. Annealed SAE-AISI H19

Both annealed 250 maraging steel and annealed SAE-AISI H19 are iron alloys. Both are furnished in the annealed condition. They have 74% of their average alloy composition in common. There are 20 material properties with values for both materials. Properties with values for just one material (10, in this case) are not shown.

For each property being compared, the top bar is annealed 250 maraging steel and the bottom bar is annealed SAE-AISI H19.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
190
Poisson's Ratio 0.3
0.29
Shear Modulus, GPa 75
75
Tensile Strength: Ultimate (UTS), MPa 970
720

Thermal Properties

Latent Heat of Fusion, J/g 270
260
Melting Completion (Liquidus), °C 1480
1540
Melting Onset (Solidus), °C 1430
1490
Specific Heat Capacity, J/kg-K 450
460
Thermal Expansion, µm/m-K 12
12

Otherwise Unclassified Properties

Base Metal Price, % relative 32
22
Density, g/cm3 8.2
8.2
Embodied Carbon, kg CO2/kg material 4.9
7.5
Embodied Energy, MJ/kg 65
110
Embodied Water, L/kg 140
110

Common Calculations

PREN (Pitting Resistance) 16
13
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 23
24
Strength to Weight: Axial, points 33
24
Strength to Weight: Bending, points 26
22
Thermal Shock Resistance, points 29
21

Alloy Composition

Aluminum (Al), % 0.050 to 0.15
0
Boron (B), % 0 to 0.0030
0
Calcium (Ca), % 0 to 0.050
0
Carbon (C), % 0 to 0.030
0.32 to 0.45
Chromium (Cr), % 0
4.0 to 4.8
Cobalt (Co), % 7.0 to 8.5
4.0 to 4.5
Copper (Cu), % 0
0 to 0.25
Iron (Fe), % 66.3 to 71.1
81.4 to 85.5
Manganese (Mn), % 0 to 0.1
0.2 to 0.5
Molybdenum (Mo), % 4.6 to 5.2
0.3 to 0.55
Nickel (Ni), % 17 to 19
0 to 0.3
Phosphorus (P), % 0 to 0.010
0 to 0.030
Silicon (Si), % 0 to 0.1
0.2 to 0.5
Sulfur (S), % 0 to 0.010
0 to 0.030
Titanium (Ti), % 0.3 to 0.5
0
Tungsten (W), % 0
3.8 to 4.5
Vanadium (V), % 0
1.8 to 2.2
Zirconium (Zr), % 0 to 0.020
0