Titanium Alloy 6-6-2 /6Al-6V-2Sn


Technical Data Sheet

Titanium 6-6-2 (6Al-6V-2Sn) is a heat treatable, high strength titanium alloy with higher strength and section hardenability that 6Al-4V. but with lower toughness and ductility and limited weldability. 6-6-2 is typically used in airframe component applications.

Chemical Composition Limits
Weight % Al Sn V Fe C N H O Others (total)
Titanium
6Al-6V-2Sn
5.0-6.0 1.50-2.50 5.0-6.0 0.35-1.0 0.05 0.04 0.015 0.20 0.30

Typical Mechanical Properties

Material Diameter Tensile Strength min Yield Strength Elongation in 4D (%) Reduction of area(%)
ksi Mpa ksi Mpa
Titanium 6Al-6V-2Sn
Bar annealed
Up to 2.0" 150 1034 140-165 965-1138 10 20
Titanium 6Al-6V-2Sn
Bar annealed
2.0" - 4.0" 145 1000 135-165 931-1103 10 15

Availability
Titanium 6Al-6V-2Sn is available in sheet, strip, plate, bar and forgings. For all stock and size availability of Titanium 6Al-6V-2Sn contact Sales.

Specifications
AMS 4918 sheet, strip, plate (annealed)
AMS 4971 bars, rings, forgings (annealed, heat treatable)
AMS 4978 bars, rings, forgings (annealed)
AMS 4979 bars, rings, forgings (annealed & precipitation heat treated)
AMS 6935 bars, forgings (solution treated & aged)
AMS 6936 bars, forgings (annealed)
AMS-T-9046 AB-3 sheet, strip, plate
AMS-T-9047 6Al-6V-2Sn bar
MIL-T-9046J AB-3 sheet, strip, plate
MIL-T-9047 6Al-6V-2Sn bar
MIL-T-9046H Type II Comp E Sheet, Strip, Plate

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Disclaimer
Every effort is made to ensure that technical specifications are accurate. However, technical specifications included herein should be used as a guideline only. All specifications are subject to change without notice.