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Annealed 250 Maraging Steel vs. Annealed SAE-AISI T15

Both annealed 250 maraging steel and annealed SAE-AISI T15 are iron alloys. Both are furnished in the annealed condition. They have 75% 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 T15.

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
76
Tensile Strength: Ultimate (UTS), MPa 970
830

Thermal Properties

Latent Heat of Fusion, J/g 270
250
Melting Completion (Liquidus), °C 1480
1690
Melting Onset (Solidus), °C 1430
1640
Specific Heat Capacity, J/kg-K 450
430
Thermal Expansion, µm/m-K 12
12

Otherwise Unclassified Properties

Base Metal Price, % relative 32
43
Density, g/cm3 8.2
8.7
Embodied Carbon, kg CO2/kg material 4.9
16
Embodied Energy, MJ/kg 65
250
Embodied Water, L/kg 140
140

Common Calculations

PREN (Pitting Resistance) 16
27
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 23
22
Strength to Weight: Axial, points 33
26
Strength to Weight: Bending, points 26
22
Thermal Shock Resistance, points 29
26

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
1.5 to 1.6
Chromium (Cr), % 0
3.8 to 5.0
Cobalt (Co), % 7.0 to 8.5
4.8 to 5.3
Copper (Cu), % 0
0 to 0.25
Iron (Fe), % 66.3 to 71.1
67.5 to 73.5
Manganese (Mn), % 0 to 0.1
0.15 to 0.4
Molybdenum (Mo), % 4.6 to 5.2
0 to 1.0
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
11.8 to 13
Vanadium (V), % 0
4.5 to 5.3
Zirconium (Zr), % 0 to 0.020
0