AMS 6935

AMS 6935
Revision: “C” issued 04/2019
Alloy: 6AL-6V-2SN
Product Forms: Titanium Bars, Forgings, and Forging Stock
Condition: Solution Heat Treated and Aged

Composition Analysis
Aluminum: 5.0 – 6.0% Carbon (Maximum): 0.05%
Vanadium: 5.0 – 6.0% Nitrogen (Maximum): 0.04%
Tin: 1.5 – 2.5% Hydrogen (Maximum): 0.015%
Iron: 0.35 – 1.0% Yttrium (Maximum): 0.005%
Copper: 0.35 – 1.0% Other Elements (Total): 0.30%
Oxygen (Maximum): 0.20% Titanium: Balance

 

Tensile Properties (Minimums)*
Tensile: 150 – 175 ksi Elongation: 6 – 8%
Yield: 155 – 170 ksi Reduction of Area: 15 – 20%

*Tensile property requirements vary based on orientation, section thickness/diameter, and cognizant engineering organization requirements.

Required Acceptance Tests

  • Chemical Composition
  • Tensile Properties
  • Microstructure
  • Surface Contamination
  • Macrostructure
  • Ultrasonic (where required)

Disclaimer
The use of this information is strictly voluntary. Information may contain typographical errors, and should be used as a guideline only. This Material Spec Sheet contains generalizations and is in no way a substitution for the AMS 6935 specification.

To purchase AMS 6935C, please visit: http://standards.sae.org/ams6935c/

Changes may be made to the information contained herein.

PERFORMANCE TITANIUM GROUP: A CUT ABOVE THE REST