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Waspaloy A Nickel Superalloy (UNS N07001)
Categories: Metal; Superalloy; Nickel Base

Material Notes: Waspaloy A has a higher solution temperature and longer time at stabilization than Waspaloy B. Typical Application: Jet engine blades

Mechanical property data for heat treated samples.

Key Words: Nimonic PK50, ATG W1, RGT 132
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Physical PropertiesMetricEnglishComments
Density 8.19 g/cc0.296 lb/in³
 
Mechanical PropertiesMetricEnglishComments
Rupture Strength  46.9 MPa
@Temperature 982 °C,
Time 360000 sec
6800 psi
@Temperature 1800 °F,
Time 100 hour
 176 MPa
@Temperature 816 °C,
Time 3.60e+6 sec
25500 psi
@Temperature 1500 °F,
Time 1000 hour
 276 MPa
@Temperature 816 °C,
Time 360000 sec
40000 psi
@Temperature 1500 °F,
Time 100 hour
 607 MPa
@Temperature 649 °C,
Time 3.60e+6 sec
88000 psi
@Temperature 1200 °F,
Time 1000 hour
 745 MPa
@Temperature 649 °C,
Time 360000 sec
108000 psi
@Temperature 1200 °F,
Time 100 hour
 
Thermal PropertiesMetricEnglishComments
CTE, linear 12.2 µm/m-°C
@Temperature 20.0 - 100 °C
6.78 µin/in-°F
@Temperature 68.0 - 212 °F
Thermal Conductivity 11.3 W/m-K
@Temperature 20.0 - 100 °C
78.3 BTU-in/hr-ft²-°F
@Temperature 68.0 - 212 °F
 
Component Elements PropertiesMetricEnglishComments
Aluminum, Al 1.4 %1.4 %
Boron, B 0.0060 %0.0060 %
Carbon, C 0.070 %0.070 %
Chromium, Cr 19.5 %19.5 %
Cobalt, Co 13.5 %13.5 %
Copper, Cu <= 0.10 %<= 0.10 %
Iron, Fe <= 2.0 %<= 2.0 %
Manganese, Mn <= 0.50 %<= 0.50 %
Nickel, Ni >= 59.304 %>= 59.304 %As Balance
Silicon, Si <= 0.50 %<= 0.50 %
Sulfur, S <= 0.030 %<= 0.030 %
Titanium, Ti 3.0 %3.0 %
Zirconium, Zr 0.090 %0.090 %

References for this datasheet.

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