Revision: “G, Amendment 2” issued 09/1986 ***Obsolete, S/S by AMS-T-9047***
Product Forms: Titanium and Titanium Alloy Bars (Rolled or Forged) and
Reforging Stock, Aircraft Quality
Please note, the MIL-T-9047 specification covers various Alloys and Conditions. This Spec Sheet is only for the Alloy and Condition listed above.
|Aluminum: 5.0 – 6.0%||Nitrogen (Maximum): 0.04%|
|Vanadium: 5.0 – 6.0%||Hydrogen (Maximum): 0.015%|
|Iron (Maximum): 0.35 – 1.0%||Yttrium (Maximum): 0.005%|
|Oxygen (Maximum): 0.20%||Other Elements (Total): 0.30%|
|Carbon (Maximum): 0.05%||Copper: 0.35 – 1.0%|
|Tin (Maximum): 1.5 – 2.5%||Titanium: Balance|
|Tensile Properties (Minimums)*|
|Tensile: 150 – 175 ksi||Elongation: 6 – 8%|
|Yield: 140 – 160 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
- Ultrasonic (where required)
- Tensile Properties
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 MIL-T-9047 specification.
To download MIL-T-9047G, please visit: https://assist.dla.mil/online/start/
Changes may be made to the information contained herein.