MIL-T-9046
Revision: “J” issued 01/1983 ***Obsolete, S/S by AMS-T-9046***
Alloy: 6AL-4V “AB-3”
Product Forms: Titanium and Titanium Alloy, Sheet, Strip, and Plate
Condition: Annealed
Please note, the MIL-T-9046 specification covers various Alloys and Conditions. This Spec Sheet is only for the Alloy and Condition listed above.
| Composition Analysis | |
|---|---|
| Aluminum: 5-6% | Carbon (Maximum): 0.05% |
| Vanadium: 5-6% | Nitrogen (Maximum): 0.04% |
| Iron: 0.35-1.0% | Hydrogen (Maximum): 0.015% |
| Tin: 1.5-2.5% | Yttrium (Maximum): 0.005% |
| Oxygen (Maximum): 0.20% | Other Elements (Total): 0.30% |
| Copper: 0.35-1.0% | Titanium: Balance |
| Tensile Properties (Minimums)* | |
|---|---|
| Tensile: 145-155 ksi | Elongation: 6 – 10% |
| Yield: 135-170 ksi | |
*Tensile property requirements vary based on orientation, section thickness, and cognizant engineering organization requirements.
Required Acceptance Tests
- Chemical Composition
- Microstructure
- Ultrasonic (where required)
- Tensile Properties
- Bend Test (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 MIL-T-9046 specification.
To download MIL-T-9046J, please visit: https://assist.dla.mil/online/start/
Changes may be made to the information contained herein.
