AS9100D ISO 9001:2015

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AS9100D ISO 9001:2015

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  • ASTM F136

    ASTM F136
    Revision: “-13” issued 2013
    Alloy: 6AL-4V Eli
    Product Forms: Titanium Alloy Strip, Sheet, Plate, Bar, Forging Bar, and Wire
    Condition: Annealed

    Composition Analysis
    Aluminum: 5.5 – 6.5%Carbon (Maximum): 0.08%
    Vanadium: 3.5 – 4.5%Nitrogen (Maximum): 0.05%
    Iron (Maximum): 0.25%Hydrogen (Maximum): 0.012%
    Oxygen (Maximum): 0.13%Titanium: Balance
    Tensile Properties (Minimums)*
    Tensile: 120 – 125 ksiElongation: 8 – 10%
    Yield: 110 – 115 ksiReduction 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
    • Bend Testing (where required)
    • 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 ASTM F136 specification.

    To purchase ASTM F136-13, please visit: http://www.astm.org/Standards/F136.htm

    Changes may be made to the information contained herein.

  • 6AL-4V Titanium

    Alternate Names: Grade 5 Titanium, 6-4 Titanium

    Description: 6AL-4V is the most common alloy of Titanium. As an alloyed Grade of Titanium, it is strengthened by the inclusion of roughly 6% Aluminum and 4% Vanadium. It is known as an alpha-beta Titanium alloy, containing both alpha and beta phases at room temperature. 6AL-4V typically comes in the Annealed condition, but it can be strengthened by heat treatment, such as Solution Treating and Aging. 6AL-4V offers good weldability. Overall, 6AL-4V exhibits high strength, light weight, and corrosion resistance, which make it an excellent choice for applications in aerospace, medical, oil and gas, marine, and recreational industries.

    Machinability: The American Iron and Steel Institute (AISI) determined a rating system of machinability of different materials. 160 Brinell B1112 steel was arbitrarily assigned a machinability rating of 100%. Using this as a comparable standard, ratings less than 100% are more challenging to machine, and ratings more than 100% are easier to machine. Titanium 6AL-4V is rated at 22% of B1112. Low cutting speeds, heavy feed rates, sharp tools, and ample cutting fluid are prescribed.

    6AL-4V Titanium is available in the following Product Forms:

    Round Bar (Rod), Rectangular Flat Bar (Block), Plate, and Sheet.

    6AL-4V Titanium is available in the following Specifications:

    AMS 4911AMS 4928AMS 4965
    AMS 4967AMS 6930AMS 6931
    AMS-T-9046 (AB-1 6AL4V)AMS-T-9047 (6AL-4V)MIL-T-9046 (AB-1 6AL-4V)
    MIL-T-9047 (6AL-4V)ASTM B348 (Grade 5)ASTM B265 (Grade 5)
    ASTM F1472DMS 1592DMS 1570
    Don’t see what you want? Call us at 888-772-8984 for a Quote on 6AL-4V Titanium, or Email us at Sales@performancetitanium.com!

    The use of this information is strictly voluntary and should be used as a guideline only. This data contains generalizations and is in no way a substitute for your own research. This information is not intended as a warranty or fitness of any application. Should you require further information about Titanium 6AL-4V Grade 5, please contact us and we will gladly refer you to additional sources.

  • 6AL-4V ELI

    Alternate Names: Grade 23 Titanium, 6-4 Eli Titanium

    Description: 6AL-4V Eli is an alloyed Grade of Titanium. It is strengthened by the inclusion of roughly 6% Aluminum and 4% Vanadium. Titanium 6AL-4V Eli (Extra-Low Interstitial) is considered a higher purity than 6AL-4V Grade 5 due to its lower inclusions of Iron, and the interstitial elements, Carbon and Oxygen. 6AL-4V Eli typically comes in the annealed condition, but can be found in beta annealed condition as well. 6AL-4V Eli Grade 23 shows high strength and toughness, as well as good corrosion resistance. It is found in aerospace applications where fracture toughness and fatigue strength are important. As a biocompatible Grade of Titanium, it is also known for its applications in medical and dental industries.

    Machinability: The American Iron and Steel Institute (AISI) determined a rating system of machinability of different materials. 160 Brinell B1112 steel was arbitrarily assigned a machinability rating of 100%. Using this as a comparable standard, ratings less than 100% are more challenging to machine, and ratings more than 100% are easier to machine. Titanium 6AL-4V Eli is rated at 22% of B1112. Low cutting speeds, heavy feed rates, sharp tools, and ample cutting fluid are prescribed.

    6AL-4V Eli Titanium  is available in the following Product Forms:
    Round Bar (Rod), Rectangular Flat Bar (Block), Plate, and Sheet.

    6AL-4V Eli Titanium is available in the following Specifications:

    AMS 4907ASTM B265 (Grade 23)AMS-T-9046 (AB-2 6AL-4V ELI)
    AMS 4930ASTM B348 (Grade 23)AMS-T-9047 (6AL-4V ELI)
    AMS 6932ASTM F136MIL-T-9046 (AB-2 6AL-4V ELI)
    MIL-T-9047 (6AL-4V ELI)
    Don’t see what you want? Call us at 888-772-8984 for a Quote on 6AL-4V Eli Grade 23 Titanium, or Email us at Sales@performancetitanium.com!

    The use of this information is strictly voluntary and should be used as a guideline only. This data contains generalizations and is in no way a substitute for your own research. This information is not intended as a warranty or fitness of any application. Should you require further information about Titanium 6AL-4V Eli Grade 23, please contact us and we will gladly refer you to additional sources.

  • 6AL-6V-2SN Titanium

    Alternate Names: 662 Titanium

    Description: 6AL-6V-2SN is an alloyed Grade of alpha-beta Titanium. 6AL-6V-2SN is similar to 6AL-4V in many ways, but exhibits higher strength properties due to additional Vanadium, Iron, and Copper. Welding is not typically recommended. 6AL-6V-2SN is often found in the Annealed condition, or heat treated to the higher strength Solution Treated & Aged condition. 6AL-6V-2SN exhibits extra high strength, and light weight. It is often used in aerospace, and oil & gas applications.

    Machinability: Low cutting speeds, heavy feed rates, sharp tools, and ample cutting fluid are prescribed.

    6AL-6V-2SN Titanium is available in the following Product Forms:
    Round Bar (Rod), Rectangular Flat Bar (Block), Sheet, and Plate.

    6AL-6V-2SN Titanium is available in the following Specifications:

    MIL-T-9047 (6AL-6V-2SN)AMS 6936AMS 4971
    AMS-T-9047 (6AL-6V-2SN)AMS 6935AMS 4978
    AMS-T-9046 (6AL-6V-2SN)AMS 4979AMS 4918
    MIL-T-9046 (6AL-6V-2SN)
    Don’t see what you want? Call us at 888-772-8984 for a Quote on 6AL-6V-2SN Titanium, or Email us at Sales@performancetitanium.com!

    The use of this information is strictly voluntary and should be used as a guideline only. This data contains generalizations and is in no way a substitute for your own research. This information is not intended as a warranty or fitness of any application. Should you require further information about Titanium 6AL-6V-2SN, please contact us and we will gladly refer you to additional sources.

  • 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
    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)*
    Tensile: 130 – 134 ksiElongation: 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.

  • MIL-T-9046 AB-2 6AL-4V ELI

    MIL-T-9046
    Revision: “J” issued 01/1983 ***Obsolete, S/S by AMS-T-9046***
    Alloy: 6AL-4V “AB-2”
    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: 5.5 – 6.5%Nitrogen (Maximum): 0.05%
    Vanadium: 3.5 – 4.5%Hydrogen (Maximum): 0.0125%
    Iron (Maximum): 0.25%Other Elements (Total): 0.30%
    Oxygen (Maximum): 0.13%Titanium: Balance
    Carbon (Maximum): 0.08%
    Tensile Properties (Minimums)*
    Tensile: 125 – 130 ksiElongation: 6 – 10%
    Yield: 115 – 120 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.

  • MIL-T-9046 CP-3 GRADE 2

    MIL-T-9046
    Revision: “J” issued 01/1983 ***Obsolete, S/S by AMS-T-9046***
    Grade: Commercially Pure Grade 2 (CP-3, 40 ksi min yield)
    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
    Carbon (Maximum): 0.08%Hydrogen (Maximum): 0.015%
    Nitrogen (Maximum): 0.05%Other Elements (Total): 0.30%
    Iron (Maximum): 0.30%Titanium: Balance
    Oxygen (Maximum): 0.20%
    Tensile Properties (Minimums)*
    Tensile: 50 ksi MinElongation: 20% Min
    Yield: 40 – 65 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.

  • MIL-T-9046 CP-1 GRADE 4

    MIL-T-9046
    Revision: “J” issued 01/1983 ***Obsolete, S/S by AMS-T-9046***
    Grade: Commercially Pure Grade 4 (CP-1, 70 ksi min yield)
    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
    Carbon (Maximum): 0.08%Hydrogen (Maximum): 0.015%
    Nitrogen (Maximum): 0.05%Other Elements (Total): 0.30%
    Iron (Maximum): 0.50%Titanium: Balance
    Oxygen (Maximum): 0.40%
    Tensile Properties (Minimums)*
    Tensile: 80 ksi MinElongation: 15% Min
    Yield: 70 – 95 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.

  • MIL-T-9046 AB-3 6AL-6V-2Sn

    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 ksiElongation: 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.

  • CP GRADE 4

    Alternate Names: CP Grade 4 Titanium, CP 4, Grade 4, CP 70

    Description: Commercially Pure (CP) Grade 4 Titanium is a grade of unalloyed titanium. CP Titanium mechanical properties are controlled by chemistry; specifically the input of Nitrogen, Oxygen and Iron which will increase strength of material. CP Grade 4 is higher in strength than CP Grades 1, 2, and 3. It is also commonly called “CP 70” which is in reference to its approximate yield strength. CP Grade 4 exhibits excellent corrosion resistance, as well as high strength. It is used in a variety of industries such as chemical, marine and aerospace.

    Machinability: Low cutting speeds, heavy feed rates, sharp tools, and ample cutting fluid are prescribed.

    CP Grade 4 Titanium is available in the following Product Forms:
    Round Bar (Rod), Plate, and Sheet

    CP Grade 4 Titanium is available in the following Specifications:

    AMS 4901ASTM B348 Grade 4AMS-T-9047 (CP-70 Grade 4)
    AMS 4921ASTM F67 Grade 4MIL-T-9046 (CP-1 Grade 4)
    ASTM B265 Grade 4AMS-T-9046 (CP-1 Grade 4)MIL-T-9047 (CP-70 Grade 4)
    Don’t see what you want? Call us at 888-772-8984 for a Quote on CP Grade 4 Titanium, or Email us at sales@performancetitanium.com!

    The use of this information is strictly voluntary and should be used as a guideline only. This data contains generalizations and is in no way a substitute for your own research. This information is not intended as a warranty or fitness of any application. Should you require further information about Titanium CP Grade 4, please contact us and we will gladly refer you to additional sources.

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