SAE Ti-5Al-2.5Sn Titanium Alloys
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This material has 5489 properties — only a subset is shown here.
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SAE Ti-5Al-2.5Sn Chemical Composition
SAE AMS T 81556A: 2001 / Titanium and Titanium Alloys, Extruded Bars and Shapes, Aircraft Quality
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SAE Ti-5Al-2.5Sn Physical Properties
Temperature
This material has 5489 properties — only a subset is shown here.
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SAE Ti-5Al-2.5Sn Heat Treatments
- Annealing:
Bars, wire, and flash welded rings shall be annealed by heating to a temperature within the range 718 to 843°C (1325 to 1550°F), holding at the selected temperature within ±14°C (±25°F) for 10 minutes to 4 hours depending on section thickness, and cooling as required. - Annealed by heating to a temperature within the range 704 to 843°C (1300 to 1550°F), holding at the selected temperature within ± 14°C (± 25°F) for a time commensurate with the thickness and the heating equipment and procedure used, and cooling. Additionaly, the product can meet the requirements after being reheated to 816°C ± 14°C (1500°F ± 25°F), held at heat for 20 minutes per 25 mm of thickness, cooled, and descaled.
SAE Ti-5Al-2.5Sn Mechanical Properties
Temperature
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SAE Ti-5Al-2.5Sn International Equivalent Materials
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Equivalence categories reflect chemical-composition and mechanical-property comparison — always verify suitability against the governing specification for your application.
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- 24Cross References
- 94Composition
- 724Mechanical Properties
- 158Physical Properties
- 7Heat Treatment
- 1Metallography
- -Machinability
- 74Stress-Strain
- 1Formability
- 1Fatigue
- 9Fracture
- 1Creep
- -Joints
- -Coatings
- 91Dimensions
- -Tribology
- 4283Corrosion
- 1Ageing
- -Weatherability
- 6Irradiation
- 14Total Suppliers