Aerospace series - Steel FE-PM1507 (X1CrNiMoAlTi12-11-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Forgings - a or D = 200 mm - Rm = 1 650 MPa
€58.00
Aerospace series - Steel FE-PM1507 (X1CrNiMoAlTi12-11-2) - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Forgings - a or D = 200 mm - Rm = 1 520 MPa
Aerospace series. Steel FE-PM1507 (X1CrNiMoAlTi12-11-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Bars. a or D = 200 mm. Rm = 1520 MPa
€165.00
Aerospace series. Steel FE-PM1506 (X1CrNiMoAlTi12-10-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Forgings. a or D = 200 mm. Rm = 1400 MPa
Aerospace series. Aluminium alloy AL-P3103-H16. Sheet and strip. 0,4 mm = a = 6 mm
Aerospace series. Aluminium alloy AL-P2024-T4 or T42. Clad sheet and strip. 0,3 mm = a = 6 mm
Aerospace series. Titanium and titanium alloys. Technical specification Pre-production production castings
€269.00
Aerospace series - Test methods for metallic materials - Determination of fatigue crack growth rates using Corner-Cracked (CC) test pieces
€142.00
Aerospace series - Titanium and titanium alloys - Technical specification - Part 008: Pre-production and production castings
€121.00
Aerospace series - Titanium and titanium alloys - Technical specification - Part 006: Pre-production and production forgings
Aerospace series - Macrostructure of titanium and titanium alloy wrought products - Part 002: Macrostructure of bar, section, forging stock and forgings; German and English version EN 2954-002:2010.
€98.32
Aerospace series - Macrostructure of titanium and titanium alloy wrought products - Part 001: General requirements; German and English version EN 2954-001:2010
€48.79
Specification for nickel-chromium-iron-titanium-niobium-aluminium heat-resisting alloy round wire with a maximum diameter of 2 mm for thread inserts (nickel base Cr 15.5, Fe 7.0, Ti 2.5, Nb/Ta 0.95, Al 0.70)
Specification for nickel-chromium-titanium-aluminium heat-resisting alloy bar and wire (maximum diameter or minor sectional dimension of 30 mm) for the manufacture of fasteners (nickel base, Cr 19.5, Ti 2.2, Al 1.4)
Aerospace series. Aluminium alloy AL-P2024-T3. Clad sheet and strip 0,3 mm = a = 6 mm
