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Annealed 250 Maraging Steel vs. Annealed SAE-AISI H24

Both annealed 250 maraging steel and annealed SAE-AISI H24 are iron alloys. Both are furnished in the annealed condition. They have 69% 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 H24.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
200
Poisson's Ratio 0.3
0.29
Shear Modulus, GPa 75
78
Tensile Strength: Ultimate (UTS), MPa 970
720

Thermal Properties

Latent Heat of Fusion, J/g 270
240
Melting Completion (Liquidus), °C 1480
1750
Melting Onset (Solidus), °C 1430
1700
Specific Heat Capacity, J/kg-K 450
420
Thermal Expansion, µm/m-K 12
12

Otherwise Unclassified Properties

Base Metal Price, % relative 32
37
Density, g/cm3 8.2
9.1
Embodied Carbon, kg CO2/kg material 4.9
6.1
Embodied Energy, MJ/kg 65
93
Embodied Water, L/kg 140
78

Common Calculations

PREN (Pitting Resistance) 16
28
Stiffness to Weight: Axial, points 13
12
Stiffness to Weight: Bending, points 23
22
Strength to Weight: Axial, points 33
22
Strength to Weight: Bending, points 26
20
Thermal Shock Resistance, points 29
22

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
0.42 to 0.53
Chromium (Cr), % 0
2.5 to 3.5
Cobalt (Co), % 7.0 to 8.5
0
Copper (Cu), % 0
0 to 0.25
Iron (Fe), % 66.3 to 71.1
78 to 82.4
Manganese (Mn), % 0 to 0.1
0.15 to 0.4
Molybdenum (Mo), % 4.6 to 5.2
0
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
0.15 to 0.4
Sulfur (S), % 0 to 0.010
0 to 0.030
Titanium (Ti), % 0.3 to 0.5
0
Tungsten (W), % 0
14 to 16
Vanadium (V), % 0
0.4 to 0.6
Zirconium (Zr), % 0 to 0.020
0