Mechanical Properties | Metric | English | Comments |
---|---|---|---|
Tensile Strength, Ultimate | 310 MPa @Temperature 871 °C |
45000 psi @Temperature 1600 °F |
Vacuum |
ATI Wah Chang Nb/Nb Alloy C-103 This alloy satisfies most rocket engine applications for temperatures up to 2700°F because of superior mechanical properties at all temperatures. Offers weight savings over many rocket engine desig.. |
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Tensile Strength, Ultimate | 310 MPa @Temperature 538 °C |
45000 psi @Temperature 1000 °F |
Vacuum |
ATI Wah Chang Nb/Nb Alloy C-103 This alloy satisfies most rocket engine applications for temperatures up to 2700°F because of superior mechanical properties at all temperatures. Offers weight savings over many rocket engine desig.. |