BS 3TA 11:2009+A1:2017
Specification for bar and section for machining of titanium-aluminium-vanadium alloy (Tensile strength 900–1 160 MPa) (Limiting ruling section 150 mm)
- Standard No.
- BS 3TA 11:2009+A1:2017
- Release Date
- 2009
- Published By
- British Standards Institution (BSI)
- Latest
- BS 3TA 11:2009+A1:2017
- Scope
- What is BS 3TA 11- Titanium-aluminium-vanadium alloy bars and sections for aerospace applications about? BS 3TA 11 is a standard that serves technical specifications for Titanium-aluminium-vanadium alloy bars and sections for aerospace applications, ensuring structural stability and longevity of parts and components. BS 3TA 11 specifies requirements for titanium-aluminium-vanadium alloy bar and section with a tensile strength of 900 MPa to 1 160 MPa. Who is BS 3TA 11- Titanium-aluminium-vanadium alloy bars and sections for aerospace applications for?
BS 3TA 11:2009+A1:2017 history
- 2009 BS 3TA 11:2009+A1:2017 Specification for bar and section for machining of titanium-aluminium-vanadium alloy (Tensile strength 900–1 160 MPa) (Limiting ruling section 150 mm)
- 2012 BS EN 3355:2012 Aerospace series. Titanium alloy TI-P64001 (Ti-6Al-4V). Annealed. Extruded section. De
150 mm. 900 MPa Rm 1160 MPa - 2009 BS 3TA 11:2009 Specification for bar and section for machining of titanium-aluminium -vanadium alloy (tensile strength 900-1160 MPa) (limiting ruling section 150 mm)
- 1974 BS 2TA 11:1974 Specification for bar and section for machining of titanium-aluminium-vanadium alloy (tensile strength 900-1160 MPa) (limiting ruling section 150 mm)
