ZEE - UNEQUAL LEG EXTRUDED (Stabilized: Mar 2012)
€68.00
I - SECTION - EXTRUDED (Stabilized: Mar 2012)
TEE - BULB SECTION EXTRUDED (Stabilized: Mar 2012)
Tolerances Rubber Products (Stabilized: Nov 2011)
€71.00
Trace Element Control Nickel Alloy, Cobalt Alloy, and Iron Alloy Wrought Products for High-Temperature, High-Stressed Applications (Stabilized: Jan 2013)
Aerospace series. Steel X5CrNiCu17-4 (1.4542). Air melted. Solution treated and precipitation treated. Sheets and strips. a = 6 mm - Rm = 930 MPa
€165.00
Aerospace series. Steel X5CrNiCu17-4 (1.4542). Air melted. Solution treated and precipitation treated. Sheets and strips. a = 6 mm. Rm = 930 MPa
Aerospace series. Steel 36NiCrMo16 (1.6773) - 1 250 MPa = Rm = 1 400 MPa. Bars - De = 75 mm
Standard Test Method for In-Plane Shear Response of Polymer Matrix Composite Materials by Tensile Test of a ±45° Laminate
€65.00
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. Steel X5CrNiCu17-4 (1.4542). Air melted. Solution treated and precipitation treated. Forgings. a or D = 200 mm. Rm = 1 310 MPa
Aerospace series. Steel X5CrNiCu17-4 (1.4542). Air melted. Solution treated and precipitation treated. Forgings. a or D = 200 mm. Rm = 930 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
Standard Test Method for Sandwich Corrosion Test
Standard Test Method for Normal Spectral Emittance at Elevated Temperatures of Nonconducting Specimens
