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Annealed 200 Maraging Steel vs. Annealed SAE-AISI H25

Both annealed 200 maraging steel and annealed SAE-AISI H25 are iron alloys. Both are furnished in the annealed condition. They have 70% 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 200 maraging steel and the bottom bar is annealed SAE-AISI H25.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
200
Poisson's Ratio 0.3
0.29
Shear Modulus, GPa 74
79
Tensile Strength: Ultimate (UTS), MPa 970
710

Thermal Properties

Latent Heat of Fusion, J/g 260
250
Melting Completion (Liquidus), °C 1460
1750
Melting Onset (Solidus), °C 1420
1700
Specific Heat Capacity, J/kg-K 460
420
Thermal Expansion, µm/m-K 12
12

Otherwise Unclassified Properties

Base Metal Price, % relative 31
38
Density, g/cm3 8.2
9.1
Embodied Carbon, kg CO2/kg material 4.5
6.2
Embodied Energy, MJ/kg 59
93
Embodied Water, L/kg 140
83

Common Calculations

PREN (Pitting Resistance) 11
29
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 27
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
0.22 to 0.32
Chromium (Cr), % 0
3.8 to 4.5
Cobalt (Co), % 8.0 to 9.0
0
Copper (Cu), % 0
0 to 0.25
Iron (Fe), % 67.8 to 71.8
77.2 to 81.3
Manganese (Mn), % 0 to 0.1
0.15 to 0.4
Molybdenum (Mo), % 3.0 to 3.5
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), % 0.15 to 0.25
0
Tungsten (W), % 0
14 to 16
Vanadium (V), % 0
0.4 to 0.6
Zirconium (Zr), % 0 to 0.020
0