Titanium 6Al-2Sn-4Zr-6Mo

Applications 

Intermediate-temperature jet engine applications. Blades, discs, spacers, seals. Standard, rotor/premium grades.

Composition nominal wt. % 

Al 6.0, C 0.10 max, Fe 0.10, H 0.015, Mo 6.0, N 0.02, O 0.12, Sn 2.0, Ti rem, Zr 4.0

Specifications 

AMS 4981.
MIL-T-9047, -83142.

Density lb/in3 (gcm3) 

0.168 (4.65)

Metallurgical Condition 

1,625°F + age

Tensile Strength ksi (MPa) 

170 (1,172)

0.2% Yield Strength ksi (MPa) 

160 (1,104) Elongation % 

10

Reduction in Area % 

15

Hardness 

38 HRC

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