Sheet nickel

Mechanical resistance: 827 MPa
Elasticity: 414 MPa
Typical elongation: 40 %

... pitting and the high level of nickel provides resistance to chloride stress corrosion cracking. The material possesses a high degree of formability and shows better weldability than many of the other highly alloyed nickel-base ...

Elasticity: 207,000 psi - 310,000 psi
Typical elongation: 30, 35 %
Length: 1,500 mm - 12,500 mm

VDM® Alloy 600 and the solution-annealed variant 600 H are nickel-chromium-iron alloys. They are characterized by: good resistance against oxidation, carbonization and nitriding, good resistance to stress corrosion ...

Typical elongation: 8 %

Tensile: 450 MPa, Yield: 350 MPa The high specific strength of magnesium alloys has great application significance in aerospace and weaponry; at the same time, some parts made of magnesium alloys also withstand changes in space temperature ...

Alloy 718 is a nickel-chromium-cobalt-molybdenum alloy with exceptional strength and oxidation resistance at high temperatures. The addition of aluminium, titanium, niobium and molybdenum gives the material superior strength. ...

Length: 120 in
Width: 36 in
Thickness: 0.02 in

Item: 15832 Shape: Sheet Temper: 0.0210 IN Thick Sheet 600 NICKEL CR, BQ, Annealed, CR 36.0000 IN Width X 120.0000 IN Length Specs: AMS.5540,ASME.SB168,DIN.EN10204,ASTM.B168,PWA.300,GE.S400,GE.S1000,PWA.MCL-F17,UNS.N06600 LBS/SFT: ...

Thickness: 0.01 in - 1.5 in

We carry a large selection of the High Temperature application aircraft sheet and plate available in a variety of specifications. AMS 5525, AMS 5530, AMS 5608, AMS 5536, AMS 5540 AMS 5596, AMS 5599, AMS 5597, AMS 5542, ...

Diameter: 0.01 in - 0.13 in

PMET 802 – Mar M 002 welding wire. Used for gas turbine engine structural components.

Mechanical resistance: 462 MPa
Elasticity: 148 MPa
Typical elongation: 47 %

Alloy 200 & Alloy 201 are nickel alloys which have been combined into one with dual certified chemistry. DUAL SOLUTION The result is an alloy which benefits from the required characteristics from both alloys in a ...