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Annealed 250 Maraging Steel vs. Annealed SAE-AISI T4

Both annealed 250 maraging steel and annealed SAE-AISI T4 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 (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 T4.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
210
Poisson's Ratio 0.3
0.29
Shear Modulus, GPa 75
80
Tensile Strength: Ultimate (UTS), MPa 970
800

Thermal Properties

Latent Heat of Fusion, J/g 270
250
Melting Completion (Liquidus), °C 1480
1810
Melting Onset (Solidus), °C 1430
1750
Specific Heat Capacity, J/kg-K 450
410
Thermal Expansion, µm/m-K 12
12

Otherwise Unclassified Properties

Base Metal Price, % relative 32
55
Density, g/cm3 8.2
9.4
Embodied Carbon, kg CO2/kg material 4.9
8.5
Embodied Energy, MJ/kg 65
130
Embodied Water, L/kg 140
120

Common Calculations

PREN (Pitting Resistance) 16
37
Stiffness to Weight: Axial, points 13
12
Stiffness to Weight: Bending, points 23
21
Strength to Weight: Axial, points 33
24
Strength to Weight: Bending, points 26
20
Thermal Shock Resistance, points 29
24

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
0.7 to 0.8
Chromium (Cr), % 0
3.8 to 4.5
Cobalt (Co), % 7.0 to 8.5
4.3 to 5.8
Copper (Cu), % 0
0 to 0.25
Iron (Fe), % 66.3 to 71.1
66.3 to 72.3
Manganese (Mn), % 0 to 0.1
0.1 to 0.4
Molybdenum (Mo), % 4.6 to 5.2
0.4 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
0.8 to 1.2
Zirconium (Zr), % 0 to 0.020
0