Aerospace series. Metallic materials. Rules for drafting and presentation of material standards Specific rules filler metals brazing
€269.00
BS EN 2002-002 Aerospace series - Metallic materials Test methods Part 2: Tensile testing at elevated temperature
€23.00
BS EN 2002-001 Aerospace series - Metallic materials Test methods Part 1: Tensile testing at ambient temperature
Aerospace series — Heat-resisting alloy X4NiCrTiMoV26-15 (1.4680) — Consumable electrode remelted — Not heat treated — Forging stock — a or D ? 250 mm
€165.00
Aerospace series — Heat-resisting alloy X6NiCrTiMoV26-15 (1.4980) — Consumable electrode remelted — Solution treated and precipitation treated — Bars and sections — a or D ? 100 mm — Rm ? 900 MPa
Aerospace series — Heat-resisting alloy X6NiCrTiMoV26-15 (1.4980) — Consumable electrode remelted — Not heat treated — Forging stock — a or D ? 200 mm
Aerospace series. Heat-resisting alloy X6NiCrTiMoV26-15 (1.4980). Consumable electrode remelted. Solution treated and precipitation treated. Bars and sections. De = 100 mm. Rm = 960 MPa
Aerospace series. Metallic materials. Definition of general terms
Aerospace series. Heat-resisting alloy X6NiCrTiMoV26-15 (1.4980). Softened and cold worked. Wires for forged fasteners. D = 15 mm. 900 MPa = Rm = 1 100 MPa
Aerospace series. Heat-resisting alloy X6NiCrTiMoV26-15 (1.4980). Consumable electrode remelted. Solution treated and precipitation treated. Sheets, strips and plates. 0,5 = a = 10 mm
Aerospace series. Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15). Non heat treated, forging stock a or D = 250 mmAerospace series. Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15). Non heat treated, forging stock a or D = 250 mmAerospace series. Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15). Non heat treated, forging stock a or D = 250 mm
Aerospace series. Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Solution treated and precipitation treated, bar and section a or D = 100 mm, Rm = 900 MPaAerospace series. Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Solution treated and precipitation treated, bar and section a or D = 100 mm, Rm = 900 MPaAerospace series. Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Solution treated and precipitation treated, bar and section a or D = 100 mm, Rm = 900 MPa
Aerospace series. Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Non heat treated, forging stock a or D = 200 mmAerospace series. Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Non heat treated, forging stock a or D = 200 mmAerospace series. Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Non heat treated, forging stock a or D = 200 mm
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 precipitation treated, bar and section De = 100 mm, Rm = 960 MPaAerospace series. Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Solution treated and precipitation treated, bar and section De = 100 mm, Rm = 960 MPa
BS EN 3873 Aerospace series — Test methods for metallic materials — Determination of fatigue crack growth rates using Corner-Cracked (CC) test pieces
