This Nickel-Chromium-Molybdenum alloy tolerates high temperatures
and gives a design freedom in areas where weld geometry makes
excessive heat build-up unavoidable. Resistance to general and localised corrosion and stress corrosion cracking is generally similar
to Hastelloy C-276.
 

Applications include:

  • Chemical Processing
Approximate Chemical Composition
Ni 65%
Cr 16%
Mo 16%
Fe 3% max
Co 2% max
DENSITY 8.64 g/cm3 0.312 lb/in3
MELTING POINT 1399oC 2550oF
COEFFICIENT OF EXPANSION 10.8 µm/m °C
( 20 - 100°C)
6.0 x 10-6 in/in °F
( 70 - 212°F)
MODULUS OF RIGIDITY 81.2 kN/m2 11777 ksi
MODULUS OF ELASTICITY 212.4 kN/m2 30807 ksi
 
CONDITION OF SUPPLY HEAT TREATMENT (AFTER FORMING)
Annealed/Spring Temper Stress relieve at 400oC - 450oC (750oF - 840oF) for 2 hours and air cool.
 
CONDITION  

APPROX TENSILE STRENGTH

 

APPROX SERVICE TEMPERATURE

Annealed 800-1100 N/mm2 116-159 ksi -200o to +400oC -330o to +750oF
Spring Temper 1300-1500 N/mm2 189-218 ksi -200o to +400oC -330o to +750oF
 
STANDARDS
ASTM B574 ASTM B619
 


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