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Titanium Ti-6Al-2Sn-4Zr-6Mo (Ti-6-2-4-6) BSTA
Categories: Metal; Nonferrous Metal; Titanium Alloy; Alpha/Beta Titanium Alloy

Material Notes: Information provided by Allvac and the references. Beta Solution Treated 985ºC, Aged 595ºC. Alpha-Beta Alloy.

Characteristics: High strength at elevated temperatures, heat-treatable, good hardenability, weldable.

Applications: Intermediate-temperature jet engine applications. Blades, discs, spacers, seals.

Forms typically available: Billet, bar, plate and sheet.

4 other heat treatments of this alloy are listed in MatWeb.

Key Words: Ti-6246; Titanium 6-2-4-6; UNS R56260
Vendors:
TITANIUM ENGINEERS is your source for high strength, NACE titanium alloys, with a full range of stock sizes and sizes made to order. Our in-house metallurgical experts ensure the best alloy selection and process titanium to meet unique customer specifications. Please visit our website www.TitaniumEngineers.com for more information or call us at +1 281 265 2910 (USA) or +44 (0) 1675 464200 (UK).

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Physical PropertiesOriginal ValueComments
Density 4.65 g/cc
 
Mechanical PropertiesOriginal ValueComments
Hardness, Brinell 360Estimated from Rockwell C.
Hardness, Knoop 392Estimated from Rockwell C.
Hardness, Rockwell C 39
Hardness, Vickers 480
Tensile Strength, Ultimate 1200 MPa
Tensile Strength, Yield 1050 MPa
Elongation at Break 7.0 %
Tensile Modulus 114 GPa
Poissons Ratio 0.33Typical for alpha-beta titanium alloy.
Shear Modulus 42.9 GPaCalculated from typical values.
 
Electrical PropertiesOriginal ValueComments
Electrical Resistivity 0.000190 ohm-cm
 
Thermal PropertiesOriginal ValueComments
CTE, linear 8.60 µm/m-°C
@Temperature 20.0 °C
 9.90 µm/m-°C
@Temperature 205 °C
 10.4 µm/m-°C
@Temperature 540 °C
Specific Heat Capacity 0.500 J/g-°C
Thermal Conductivity 7.70 W/m-K
@Temperature 23.0 °C
 13.5 W/m-K
@Temperature 540 °C
Melting Point 1595 - 1675 °C
Solidus 1595 °C
Liquidus 1675 °C
Beta Transus 935 °C
 
Component Elements PropertiesOriginal ValueComments
Aluminum, Al 6.0 %
Carbon, C <= 0.040 %
Iron, Fe <= 0.15 %
Molybdenum, Mo 6.0 %
Nitrogen, N <= 0.040 %
Oxygen, O <= 0.12 %
Tin, Sn 2.0 %
Titanium, Ti 82 %
Zirconium, Zr 4.0 %

References for this datasheet.

Some of the values displayed above may have been converted from their original units and/or rounded in order to display the information in a consistent format. Users requiring more precise data for scientific or engineering calculations can click on the property value to see the original value as well as raw conversions to equivalent units. We advise that you only use the original value or one of its raw conversions in your calculations to minimize rounding error. We also ask that you refer to MatWeb's terms of use regarding this information. Click here to go back to viewing the property data in MatWeb's normal format.

Users viewing this material also viewed the following:
Titanium Ti-6Al-2Sn-4Zr-6Mo (Ti-6-2-4-6) STA-1
Titanium Ti-6Al-2Sn-4Zr-6Mo (Ti-6-2-4-6) STOA
Titanium Ti-6Al-2Sn-4Zr-6Mo (Ti-6-2-4-6) STA-2
Titanium Ti-6Al-2Sn-4Zr-6Mo (Ti-6-2-4-6) Annealed
ATI Allvac® 6-2-4-6 Titanium Alloy, Heat Treatment: 885°C (1625°F) + Age

MTP623 / 14236

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