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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 40:2009 Specification for bar for machining of titanium- aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1205-1375 MPa) (limiting ruling section over 25 mm up to and including 75 mm)
immediate downloadReleased: 2009-11-30
BS 2TA 40:2009 Specification for bar for machining of titanium- aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1205-1375 MPa) (limiting ruling section over 25 mm up to and including 75 mm)

BS 2TA 40:2009

Specification for bar for machining of titanium- aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1205-1375 MPa) (limiting ruling section over 25 mm up to and including 75 mm)

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Standard number:BS 2TA 40:2009
Pages:10
Released:2009-11-30
ISBN:978 0 580 65365 0
Status:Standard
DESCRIPTION

BS 2TA 40:2009


This standard BS 2TA 40:2009 Specification for bar for machining of titanium- aluminium-molybdenum-tin-silicon-carbon alloy (tensile strength 1205-1375 MPa) (limiting ruling section over 25 mm up to and including 75 mm) is classified in these ICS categories:
  • 49.025.30 Titanium

This British Standard specifies requirements for titanium-aluminium-molybdenum-tin-silicon-carbon alloy bar with a tensile strength of 1 205 MPa to 1 375 MPa.


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