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Annealed 250 Maraging Steel vs. Annealed SAE-AISI T2

Both annealed 250 maraging steel and annealed SAE-AISI T2 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 (11, 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 T2.

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
79
Tensile Strength: Ultimate (UTS), MPa 970
780

Thermal Properties

Latent Heat of Fusion, J/g 270
250
Melting Completion (Liquidus), °C 1480
1820
Melting Onset (Solidus), °C 1430
1760
Specific Heat Capacity, J/kg-K 450
410
Thermal Expansion, µm/m-K 12
12

Otherwise Unclassified Properties

Base Metal Price, % relative 32
46
Density, g/cm3 8.2
9.3
Embodied Carbon, kg CO2/kg material 4.9
11
Embodied Energy, MJ/kg 65
170
Embodied Water, L/kg 140
98

Common Calculations

PREN (Pitting Resistance) 16
36
Stiffness to Weight: Axial, points 13
12
Stiffness to Weight: Bending, points 23
21
Strength to Weight: Axial, points 33
23
Strength to Weight: Bending, points 26
20
Thermal Shock Resistance, points 29
23

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
0.8 to 0.9
Chromium (Cr), % 0
3.8 to 4.5
Cobalt (Co), % 7.0 to 8.5
0
Copper (Cu), % 0
0 to 0.25
Iron (Fe), % 66.3 to 71.1
70.8 to 75.8
Manganese (Mn), % 0 to 0.1
0.2 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
0.2 to 0.4
Sulfur (S), % 0 to 0.010
0 to 0.030
Titanium (Ti), % 0.3 to 0.5
0
Tungsten (W), % 0
17.5 to 19
Vanadium (V), % 0
1.8 to 2.4
Zirconium (Zr), % 0 to 0.020
0