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ASTM A387 Grade 91 Class 2 vs. ISO-WD32350 Magnesium

ASTM A387 grade 91 class 2 belongs to the iron alloys classification, while ISO-WD32350 magnesium belongs to the magnesium alloys. There are 30 material properties with values for both materials. Properties with values for just one material (2, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.

For each property being compared, the top bar is ASTM A387 grade 91 class 2 and the bottom bar is ISO-WD32350 magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
45
Elongation at Break, % 20
5.7 to 10
Fatigue Strength, MPa 330
120 to 130
Poisson's Ratio 0.28
0.29
Shear Modulus, GPa 75
18
Shear Strength, MPa 420
150 to 170
Tensile Strength: Ultimate (UTS), MPa 670
250 to 290
Tensile Strength: Yield (Proof), MPa 470
140 to 180

Thermal Properties

Latent Heat of Fusion, J/g 270
340
Maximum Temperature: Mechanical, °C 600
95
Melting Completion (Liquidus), °C 1460
600
Melting Onset (Solidus), °C 1420
560
Specific Heat Capacity, J/kg-K 470
990
Thermal Conductivity, W/m-K 26
130
Thermal Expansion, µm/m-K 13
25

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 8.9
25
Electrical Conductivity: Equal Weight (Specific), % IACS 10
130

Otherwise Unclassified Properties

Base Metal Price, % relative 7.0
12
Density, g/cm3 7.8
1.7
Embodied Carbon, kg CO2/kg material 2.6
23
Embodied Energy, MJ/kg 37
160
Embodied Water, L/kg 88
960

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 120
14 to 23
Resilience: Unit (Modulus of Resilience), kJ/m3 580
210 to 380
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 25
68
Strength to Weight: Axial, points 24
39 to 46
Strength to Weight: Bending, points 22
50 to 55
Thermal Diffusivity, mm2/s 6.9
73
Thermal Shock Resistance, points 19
16 to 18

Alloy Composition

Aluminum (Al), % 0 to 0.020
0 to 0.1
Carbon (C), % 0.080 to 0.12
0
Chromium (Cr), % 8.0 to 9.5
0
Copper (Cu), % 0
0 to 0.1
Iron (Fe), % 87.3 to 90.3
0 to 0.060
Magnesium (Mg), % 0
95.7 to 97.7
Manganese (Mn), % 0.3 to 0.6
0.6 to 1.3
Molybdenum (Mo), % 0.85 to 1.1
0
Nickel (Ni), % 0 to 0.4
0 to 0.0050
Niobium (Nb), % 0.060 to 0.1
0
Nitrogen (N), % 0.030 to 0.070
0
Phosphorus (P), % 0 to 0.020
0
Silicon (Si), % 0.2 to 0.5
0 to 0.1
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0 to 0.010
0
Vanadium (V), % 0.18 to 0.25
0
Zinc (Zn), % 0
1.8 to 2.3
Zirconium (Zr), % 0 to 0.010
0
Residuals, % 0
0 to 0.3