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Titanium Ti-4Al-4Mo-2Sn-0.5Si (IMI550), STA
Categories: Metal; Nonferrous Metal; Titanium Alloy; Alpha/Beta Titanium Alloy

Material Notes: Solution Treated 900ºC, Aged 500ºC. Alpha-Beta Alloy, medium strength.

Applications: Aerospace - airframe and engine components.

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Physical PropertiesOriginal ValueComments
Density 4.57 g/cc
 
Mechanical PropertiesOriginal ValueComments
Hardness, Vickers 360
Tensile Strength, Ultimate 1100 MPa
Tensile Strength, Yield 940 MPa
Elongation at Break 7.0 %
Modulus of Elasticity 115 GPa
Tensile Modulus 96.0 GPa
@Temperature 400 °C
 107 GPa
@Temperature 200 °C
Notched Tensile Strength 1410 MPaKt (stress concentration factor) = 3
Poissons Ratio 0.33Typical for alpha-beta titanium alloy.
Fatigue Strength 330 MPa
@# of Cycles 1.00e+7
notched
 390 MPa
@# of Cycles 20000
Kt (stress concentration factor) = 3
 820 MPa
@# of Cycles 1.00e+7
unnotched
 1100 MPa
@# of Cycles 2000
Unnotched
Fracture Toughness 60.0 MPa-m½
Shear Modulus 43.2 GPaCalculated from typical values.
Charpy Impact 23.0 JU-Notch
 
Electrical PropertiesOriginal ValueComments
Electrical Resistivity 0.000159 ohm-cm
 0.000170 ohm-cm
@Temperature 200 °C
 
Thermal PropertiesOriginal ValueComments
CTE, linear 8.80 µm/m-°C
@Temperature 20.0 - 100 °C
 9.20 µm/m-°C
@Temperature 20.0 - 315 °C
average
 9.70 µm/m-°C
@Temperature 20.0 - 500 °C
Specific Heat Capacity 0.500 J/g-°CEstimated from similar materials
Thermal Conductivity 7.50 W/m-K
 9.50 W/m-K
@Temperature 200 °C
Melting Point <= 1650 °CEstimated from similar materials
Liquidus 1650 °CEstimated from similar materials
Beta Transus 975 °C
 
Component Elements PropertiesOriginal ValueComments
Aluminum, Al 4.0 %
Hydrogen, H <= 0.0125 %
Iron, Fe <= 0.20 %
Molybdenum, Mo 4.0 %
O + 2N <= 0.27 %
Silicon, Si 0.50 %
Tin, Sn 2.0 %
Titanium, Ti 89 %

References for this datasheet.

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MTP551 / 14233

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