A Nickel-Chromium-Cobalt alloy being precipitation hardenable, having
high stress-rupture strength and creep resistance at high temperatures
up to about 950OC (1740OF). It is widely used and a well proven alloy in high temperature conditions.

Applications include:

  • Aerospace Industry
  • High Temperature Springs and Various
  • Thermal Processing

Spacer

Approximate Chemical Composition
Ni 54% min
Cr 18-21%
Co 15-21%
Ti 2-3%
Al 1-2%
DENSITY   8.18 g/cm3 0.296 lb/in3
MELTING POINT   1370oC 2500oF
COEFFICIENT OF EXPANSION   12.7 µm/m °C
( 20 - 100°C)
7.1 x 10-6 in/in °F
( 70 - 212°F)
MODULUS OF RIGIDITY   82.5 kN/m2 11966 ksi
MODULUS OF ELASTICITY *
**
213 kN/m2
227 / 240 kN/m2
30894 ksi
32924 / 34810 ksi
* Solution Annealed + Aged **Spring Temper and Aged
CONDITION OF SUPPLY HEAT TREATMENT (AFTER FORMING)
Solution Annealed Age harden at 750oC (1380oF) for 4 hours and air cool. *
Spring Temper Age harden at 650oC (1200oF) for 4 hours and air cool. *
Spring Temper Age harden at 600oC (1110oF) for 16 hours and air cool. *
 
CONDITION  

APPROX TENSILE STRENGTH

 

APPROX SERVICE TEMPERATURE

Solution Annealed 800-1000 N/mm2 116-145 ksi - -
Solution Annealed + Aged 1300-1400 N/mm2 189-203 ksi up to 550oC up to 1020oF
Spring Temper 1300-1500 N/mm2 189-218 ksi - -
Spring Temper + Aged 1500-1800 N/mm2 218-261 ksi up to 350oC up to 660oF
 
STANDARDS
BS HR 501
(Spring temper)
BS HR 502
(Solution Annealed)
BS HR 503 BS 3075 NA19 AMS 5829 NCK20TA
 
Spacer


Spacer
Spacer