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Homepage>BS Standards>49 AIRCRAFT AND SPACE VEHICLE ENGINEERING>49.025 Materials for aerospace construction>49.025.30 Titanium>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)
immediate downloadReleased: 2017-03-31
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)

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)

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Standard number:BS 3TA 11:2009+A1:2017
Pages:12
Released:2017-03-31
ISBN:978 0 580 95570 9
Status:Standard
DESCRIPTION

BS 3TA 11:2009+A1:2017


This standard 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) is classified in these ICS categories:
  • 49.025.30 Titanium

This British Standard specifies requirements for titanium-aluminium-vanadium alloy bar and section with a tensile strength of 900 MPa to 1 160 MPa.


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