Aerospace series - Non-metallic materials - Epoxy surfacing films
€69.91
Aerospace series - Non-metallic materials; rules for drafting and presentation of material standards - Part 11: Preimpregnates.
€173.74
Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4), air melted, solution treated and precipitation treated - Forgings, a or D 200 mm, R 965 MPa; Inactive for new design
€77.20
Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4), consumable electrode remelted, solution treated and precipitation treated - Sheet and strip, a 6 mm, R 1310 MPa; Inactive for new design
Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4), consumable electrode remelted, solution treated and precipitation treated - Bar, a or D 200 mm, R 1310 MPa; Inactive for new design
Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4), consumable electrode remelted, solution treated and precipitation treated - Forgings, a or D 200 mm, R 1310 MPa; Inactive for new design
Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4), air melted, solution treated and precipitation treated - Sheet and strip, a 6 mm, R 930 MPa
Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4), air melted, softened - Forging stock, a or D 300 mm
Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4), air melted, solution treated and precipitation treated - Forgings, a or D 200 mm, R 1310 MPa
Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4), air melted, solution treated and precipitation treated - Forgings, a or D 200 mm, R 930 MPa
Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4), air melted, solution treated and precipitation treated - Bar, a or D 200 mm, R 1310 MPa
Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4), air melted, solution treated and precipitation treated - Bar, a or D 200 mm, R 930 MPa
Metallic materials - Test methods - Part 6 : Bend testing
€76.10
Standard Test Method for Explosive Reactivity of Lubricants with Aerospace Alloys Under High Shear (Withdrawn 2019)
This product is not for sale, please contact us for more information
Standard Test Method for Explosive Reactivity of Lubricants with Aerospace Alloys Under High Shear