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>BSI Standards >49 AIRCRAFT AND SPACE VEHICLE ENGINEERING>49.025 Materials for aerospace construction>49.025.30 Titanium>BS 2TA 56:2009 Specification for plate of titanium-aluminium-vanadium alloy (tensile strength 895-1150 MPa) (maximum thickness 100 mm)
immediate downloadReleased: 2009-11-30
BS 2TA 56:2009 Specification for plate of titanium-aluminium-vanadium alloy (tensile strength 895-1150 MPa) (maximum thickness 100 mm)

BS 2TA 56:2009

Specification for plate of titanium-aluminium-vanadium alloy (tensile strength 895-1150 MPa) (maximum thickness 100 mm)

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Standard number:BS 2TA 56:2009
Pages:10
Released:2009-11-30
ISBN:978 0 580 65462 6
Status:Standard
DESCRIPTION

BS 2TA 56:2009


This standard BS 2TA 56:2009 Specification for plate of titanium-aluminium-vanadium alloy (tensile strength 895-1150 MPa) (maximum thickness 100 mm) is classified in these ICS categories:
  • 49.025.30 Titanium

This standard specifies requirements for titanium-aluminium-vanadium alloy plate with a tensile strength of 895 to 1 150 MPa.


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