Aerospace series. Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Solution treated and precipitation treated, bar and section De ≤ 100 mm, Rm ≤ 960 MPaAerospace series. Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Solution treated and… PAS 015 Those wishing to claim conformance

Those wishing to claim conformance with BS 8848 can do so through self-declaration

This International Standard gives specifications for the angular coordinate system to be used in the design of scales

1   This International Standard specifies two methods (method A and method B) for the determination of the tensile-impact strength of plastics under defined conditions

3 Hybrid welding processes

aerospace manufacturers have started investigating alternatives to aluminum

Aerospace series. Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Solution treated and precipitation treated, bar and section De ≤ 100 mm, Rm ≤ 960 MPaAerospace series. Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Solution treated and… PAS 015 Those wishing to claim conformance1 Scope This standard specifies the requirements relating to: Heat resisting alloy FE PA2601 (X6NiCrTiMoV26 15) Solution treated and precipitation treated, bar and section De 100 mm, Rm 960 MPa for aerospace applications.