Base Element Ni(Nickel)
|Ultimate Tensile Strength (UTS)||1250 MPa|
|0.2% Proof Stress||780 MPa|
Bar: 8h/1080 degs C/AC+16h/700 degs C/AC
Three stage heat treatment for service up to 600 degs C only.
Their ability to withstand very high temperatures makes them idea for use in aircraft parts and gas turbine components, including turbine blades and exhaust nozzles.
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