Rod and Round Bar

AMS 4930
Revision: “-M” issued 11/2025
Alloy: 6AL-4V Eli
Product Forms: Titanium Alloy Bars, Wire, Forgings, and Rings
Condition: Annealed

Composition Analysis
Aluminum: 5.5 – 6.5%	Nitrogen (Maximum): 0.05%
Vanadium: 3.5 – 4.5%	Hydrogen (Maximum): 0.0125%
Iron (Maximum): 0.25%	Other Elements (Each): .10%
Oxygen (Maximum): 0.13%	Other Elements (Total): .40%
Carbon (Maximum): 0.08%	Titanium: Balance

Tensile Properties (Minimums)*
Tensile: 117 – 125 ksi	Elongation: 8 – 10%
Yield: 108 – 115 ksi	Reduction of Area: 15 – 25%

*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

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 4930 specification.

To purchase AMS 4930M, please visit: http://standards.sae.org/ams4930m/

Changes may be made to the information contained herein.

ASTM B348 Grade 23
Revision: “-25” issued 2025
Alloy: 6AL-4V ELI (Grade 23)
Product Forms: Titanium and Titanium Alloy Bars and Billets

Please note, the ASTM B348 specification covers various Alloys. This Spec Sheet is only for the Alloy listed above.

Composition Analysis
Aluminum: 5.5 – 6.5%	Nitrogen (Maximum): 0.03%
Vanadium: 3.5 – 4.5%	Hydrogen (Maximum): 0.0125%
Iron (Maximum): 0.25%	Other Elements (Maximum, Each): 0.10%
Oxygen (Maximum): 0.13%	Other Elements (Total): 0.40%
Carbon (Maximum): 0.08%	Titanium: Balance

Tensile Properties (Minimums)*
Tensile: 120 ksi	Elongation: 10% min
Yield: 110 ksi	Reduction of Area: 25%

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

Required Acceptance Tests

• Chemical Composition
• Tensile Properties

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 ASTM B348 specification.

To purchase ASTM B348, please visit: http://www.astm.org/Standards/B348.htm

Changes may be made to the information contained herein.

ASTM B348 Grade 2
Revision: “-25” issued 2025
Grade: Commercially Pure Grade 2
Product Forms: Titanium and Titanium Alloy Bars and Billets

Please note, the ASTM B348 specification covers various Alloys. This Spec Sheet is only for the Alloy listed above.

Composition Analysis
Iron (Maximum): 0.30%	Hydrogen (Maximum): 0.015%
Oxygen (Maximum): 0.25%	Other Elements (Maximum, Each): 0.10%
Carbon (Maximum): 0.08%	Other Elements (Total): 0.40%
Nitrogen (Maximum): 0.03%	Titanium: Balance

Tensile Properties (Minimums)*
Tensile: 50 ksi	Elongation: 20%
Yield: 40 ksi	Reduction of Area: 30%

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

Required Acceptance Tests

• Chemical Composition
• Tensile Properties

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 ASTM B348 specification.

To purchase ASTM B348, please visit: http://www.astm.org/Standards/B348.htm

Changes may be made to the information contained herein.

ASTM B348 Grade 4
Revision: “-25” issued 2025
Grade: Commercially Pure Grade 4
Product Forms: Titanium and Titanium Alloy Bars and Billets

Please note, the ASTM B348 specification covers various Alloys. This Spec Sheet is only for the Alloy listed above.

Composition Analysis
Iron (Maximum): 0.50%	Hydrogen (Maximum): 0.015%
Oxygen (Maximum): 0.40%	Other Elements (Maximum, Each): 0.10%
Carbon (Maximum): 0.08%	Other Elements (Total): 0.40%
Nitrogen (Maximum): 0.05%	Titanium: Balance

Tensile Properties (Minimums)*
Tensile: 80 ksi	Elongation: 15%
Yield: 70 ksi	Reduction of Area: 25%

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

Required Acceptance Tests

• Chemical Composition
• Tensile Properties

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 ASTM B348 specification.

To purchase ASTM B348, please visit: http://www.astm.org/Standards/B348.htm

Changes may be made to the information contained herein.

AMS 4978
Revision: “J” issued 05/2022
Alloy: 6AL-6V-2SN
Product Forms: Titanium Bars, Forgings, and Rings
Condition: Annealed

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): 0.40%
Oxygen (Maximum): 0.20%	Titanium: Balance

Tensile Properties (Minimums)*
Tensile: 145-150 ksi	Elongation: 8 – 10%
Yield: 135-165 ksi	Reduction of Area: 15 – 20%

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

Required Acceptance Tests

• Tensile Properties
• Microstructure
• Surface Contamination
• Fracture Toughness (when specified)
• Chemical Composition

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 4978 specification.

To purchase AMS 4978J, please visit: http://standards.sae.org/ams4978j/

Changes may be made to the information contained herein.

AMS 4967
Revision: “N” issued 08/2022
Alloy: 6AL-4V
Product Forms: Titanium Alloy, Bars, Wire, Forgings, and Rings
Condition: Annealed, Heat Treatable

Composition Analysis
Aluminum: 5.5 – 6.75%	Nitrogen (Maximum): 0.05%
Vanadium: 3.5 – 4.5%	Hydrogen (Maximum): 0.0125%
Iron (Maximum): 0.30%	Yttrium (Maximum): 0.005%
Oxygen (Maximum): 0.20%	Other Elements (Total): 0.40%
Carbon (Maximum): 0.08%	Titanium: Balance

Tensile Properties (Minimums)*
Tensile: 130 – 165 ksi	Elongation: 6 – 10%
Yield: 120 – 155 ksi	Reduction of Area: 20 – 25%

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

Required Acceptance Tests

• Chemical Composition
• Tensile Properties (after Heat Treat)
• Microstructure
• Surface Contamination

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 4967 specification.

To purchase AMS 4967N, please visit: https://www.sae.org/standards/content/ams4967n/

Changes may be made to the information contained herein.

AMS 4965
Revision: “N” issued 08/2022
Alloy: 6AL-4V
Product Forms: Titanium Alloy, Bars, Wire, Forgings, and Rings
Condition: Solution Heat Treated and Aged

Composition Analysis
Aluminum: 5.5 – 6.75%	Nitrogen (Maximum): 0.05%
Vanadium: 3.5 – 4.5%	Hydrogen (Maximum): 0.0125%
Iron (Maximum): 0.30%	Yttrium (Maximum): 0.005%
Oxygen (Maximum): 0.20%	Other Elements (Total): 0.40%
Carbon (Maximum): 0.08%	Titanium: Balance

Tensile Properties (Minimums)*
Tensile: 130 – 165 ksi	Elongation: 6 – 10%
Yield: 120 – 155 ksi	Reduction of Area: 20 – 25%

*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
• Fracture Toughness (when specified)

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 4965 specification.

To purchase AMS 4965N, please visit: https://www.sae.org/standards/content/ams4965n/

Changes may be made to the information contained herein.

AMS 6930
Revision: “G” issued 08/2022
Alloy: 6AL-4V
Product Forms: Titanium Alloy Bars, Forgings, and Forging Stock
Condition: Solution Heat Treated and Aged

Composition Analysis
Aluminum: 5.5 – 6.75%	Nitrogen (Maximum): 0.05%
Vanadium: 3.5 – 4.5%	Hydrogen (Maximum): 0.0125%
Iron (Maximum): 0.30%	Yttrium (Maximum): 0.005%
Oxygen (Maximum): 0.20%	Other Elements (Total): 0.40%
Carbon (Maximum): 0.08%	Titanium: Balance

Tensile Properties (Minimums)*
Tensile: 130 – 165 ksi	Elongation: 6 – 10%
Yield: 120 – 155 ksi	Reduction of Area: 10 – 25%

*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 6930 specification.

To purchase AMS 6930G, please visit: https://www.sae.org/standards/content/ams6930g/

Changes may be made to the information contained herein.