NI SPAN C Alloy 902

Material Data Sheet

Ni Span C902 Sheet is a precipitation hardenable Ni-Fe alloy attaining controlled thermoelastic coefficient and static elastic modulus at temperatures from -50oF to 150oF. The main constituents of alloy are iron, nickel and chromium with nominal traces of titanium and aluminum. It produces a reddish brown oxide layer upon exposure to natural conditions and has nominal expansion after hot and cold processing.

Alloy C902 is hardened by cold and hot processing. It can be joined through welding, brazing and soldering. The brazing should be done in heat processed form to avoid rupturing. For the great welding results, it is welded by using the techniques similar to stainless steels. Autogeneous inert gas fusion welding is preferred. While joining process, the temperature and period of joining should be taken into account because of its influence on the thermoelastic properties of the material.

Chemical Composition
Element Content (%)
Iron, Fe 47.0
Nickel, Ni 41.0 – 43.5
Chromium, Cr 4.90 – 5.75
Titanium, Ti 2.20 – 2.75
Silicon, Si 1.0
Manganese, Mn 0.80
Aluminum, Al 0.30 – 0.80
Carbon, C 0.06
Phosphorous, P 0.04
Sulfur, S 0.04
Physical Properties
Properties Metric Imperial
Density 8.05 g/cc 0.291 lb/in³
Melting Point 1450 – 1480 °C 2640 – 2700 °F
Specific Heat Capacity 0.500 J/g-°C 0.120 BTU/lb-°F
MechanicalProperties
Properties Metric Imperial
Tensile Strength, Ultimate 1210 MPa 175000 psi
Tensile Strength, Yield 760 MPa 110000 psi
Elongation at Break 25% 25%
Modulus of Elasticity 165 – 200 GPa 23900 – 290000 ksi
Shear Modulus 62.0 – 69.0 GPa 8990 – 10000 ksi
Specifications
  • AMS 5221
  • AMS 5223
  • AMS 5225
Applications
  • FGD Scrubbers
  • Reverse Osmosis
  • Distillation Columns
  • Offshore Oil and Gas
  • Heat Exchangers

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