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Homepage>BS Standards>49 AIRCRAFT AND SPACE VEHICLE ENGINEERING>49.025 Materials for aerospace construction>49.025.30 Titanium>BS 2TA 57:2009 Specification for plate of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1030-1220 MPa) (thickness over 50 mm up to and including 65 mm)
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immediate downloadReleased: 2009-11-30
BS 2TA 57:2009 Specification for plate of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1030-1220 MPa) (thickness over 50 mm up to and including 65 mm)

BS 2TA 57:2009

Specification for plate of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1030-1220 MPa) (thickness over 50 mm up to and including 65 mm)

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Standard number:BS 2TA 57:2009
Pages:10
Released:2009-11-30
ISBN:978 0 580 65463 3
Status:Standard
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BS 2TA 57:2009


This standard BS 2TA 57:2009 Specification for plate of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1030-1220 MPa) (thickness over 50 mm up to and including 65 mm) is classified in these ICS categories:
  • 49.025.30 Titanium

This standard specifies requirements for titanium-aluminium-molybdenum-tin-silicon alloy plate of a thickness over 50 mm up to and including 65 mm, with a tensile strength of 1 030 to 1220 MPa.