Titanium 6Al-6V-2Sn

Applications 

Airframes, jet engines, rocket engine cases, nuclear reactor compoenets, ordnance components.

Composition nominal wt. % 

Al 5.5, C 0.05, Cu 0.5, Fe 0.5, H 0.015 max, N 0.02, O 0.12, Sn 2.0, Ti rem, v 5.5

Specifications 

AMS 4918, 4936, 4937, 4971, 4978, 4979.
MIL-T-9047, -81556; DMS 1879, 1870, 1887.

Density lb/in3 (gcm3) 

0.164 (4.54)

Metallurgical Condition 

1,325°F anneal

Tensile Strength ksi (MPa) 

140 (966)

0.2% Yield Strength ksi (MPa) 

130 (897) Elongation % 

15

Reduction in Area % 

35

Hardness 

35 HRC

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