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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 49:2009 Specification for bar and section for machining of titanium-aluminium- molybdenum-tin-silicon-carbon alloy (Tensile strength 1000-1200 MPa) (Limiting ruling section over 100 mm up to and including 150 mm)
immediate downloadReleased: 2009-11-30
BS 2TA 49:2009 Specification for bar and section for machining of titanium-aluminium- molybdenum-tin-silicon-carbon alloy (Tensile strength 1000-1200 MPa) (Limiting ruling section over 100 mm up to and including 150 mm)

BS 2TA 49:2009

Specification for bar and section for machining of titanium-aluminium- molybdenum-tin-silicon-carbon alloy (Tensile strength 1000-1200 MPa) (Limiting ruling section over 100 mm up to and including 150 mm)

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Standard number:BS 2TA 49:2009
Pages:10
Released:2009-11-30
ISBN:978 0 580 65372 8
Status:Standard
DESCRIPTION

BS 2TA 49:2009


This standard BS 2TA 49:2009 Specification for bar and section for machining of titanium-aluminium- molybdenum-tin-silicon-carbon alloy (Tensile strength 1000-1200 MPa) (Limiting ruling section over 100 mm up to and including 150 mm) is classified in these ICS categories:
  • 49.025.30 Titanium

This standard specifies requirements for titanium-aluminium-molybdenum-tin-silicon alloy bar and section with a tensile strength of 1 000 MPa to 1 200 MPa.


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