MIL-T-9046 AB-1 6AL-4V
MIL-T-9046
Revision: “J” issued 01/1983 ***Obsolete, S/S by AMS-T-9046***
Alloy: 6AL-4V “AB-1”
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 | |
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Aluminum: 5.5 – 6.75% | Nitrogen (Maximum): 0.05% |
Vanadium: 3.5 – 4.5% | Hydrogen (Maximum): 0.0125% |
Iron (Maximum): 0.30% | Other Elements (Maximum, Each): 0.10% |
Oxygen (Maximum): 0.20% | Other Elements (Total): 0.40% |
Carbon (Maximum): 0.08% | Titanium: Balance |
Tensile Properties (Minimums)* | |
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Tensile: 130 – 134 ksi | Elongation: 8 – 10% |
Yield: 120 – 126 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.