STRESS-RUPTURE AND CREEP PROPERTIES OF HASTELLOY X MATERIAL IN AIR AND LIQUID MEDIA
Technical Report
·
OSTI ID:4799748
Creep rupture data were obtained on Hastelloy X in sheet, plate, and bar form. Test temperatures of 1350, 1500, and 1650 deg F were used. Creep and stress-rupture were determined in air, salt, and liquid metal. The data are presented in graph form. (M.C.G.)
- Research Organization:
- Pratt and Whitney Aircraft Div., United Aircraft Corp., Hartford, Conn.
- DOE Contract Number:
- AT(11-1)-229
- NSA Number:
- NSA-16-013588
- OSTI ID:
- 4799748
- Report Number(s):
- TIM-287
- Country of Publication:
- United States
- Language:
- English
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