FANSTEEL 82

Alloy Digest ◽  
1963 ◽  
Vol 12 (2) ◽  

Abstract Fansteel 82 is a columbium base alloy having superior high temperature strength while retaining the good fabricability of pure columbium. Fansteel 82 exhibits superior resistance to oxidation at temperatures above 1800 F; however, a protective coating will be necessary except for only very short time applications. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Cb-3. Producer or source: Fansteel Metallurgical Corporation.

Alloy Digest ◽  
1972 ◽  
Vol 21 (7) ◽  

Abstract UDIMET 105 is a nickel-base alloy which was developed for service at elevated temperatures. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-175. Producer or source: Special Metals Corporation.


Alloy Digest ◽  
1972 ◽  
Vol 21 (4) ◽  

Abstract UDIMET 75 is a nickel-base high-temperature alloy developed for good resistance to oxidation and scaling to 2000 F. It can be fabricated and welded readily. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-171. Producer or source: Special Metals Corporation.


Alloy Digest ◽  
1965 ◽  
Vol 14 (6) ◽  

Abstract Columbium D43 is a columbium-base alloy with inhibited grain growth during prolonged exposure at high temperature. It is recommended for high temperature service. This datasheet provides information on composition, physical properties, microstructure, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Cb-9. Producer or source: E. I. Dupont de Nemours & Company Inc..


Alloy Digest ◽  
1962 ◽  
Vol 11 (10) ◽  

Abstract COLUMBIUM D-14 is a readily fabricable, moderate strength columbium base alloy for high temperature service. It is double consumable-electrode vacuum are melted. This datasheet provides information on composition, physical properties, microstructure, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance as well as heat treating, machining, joining, and surface treatment. Filing Code: Cb-2. Producer or source: E. I. Dupont de Nemours & Company Inc..


Alloy Digest ◽  
1954 ◽  
Vol 3 (1) ◽  

Abstract Ti-150A is a titanium-base alloy containing iron and chromium. It is used primarily in bars and forgings. It is heat treatable and work-hardenable. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength as well as fracture toughness. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ti-2. Producer or source: Titanium Metals Corporation of America.


Alloy Digest ◽  
1971 ◽  
Vol 20 (12) ◽  

Abstract PYROTOOL V is an austenitic precipitation-hardenable iron-base alloy designed to display high-strength properties at temperatures up to 1300 F (704 C). This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Fe-49. Producer or source: Carpenter.


Alloy Digest ◽  
1966 ◽  
Vol 15 (3) ◽  

Abstract FIRTH FS-718 is an austenitic nickel-base alloy having good cryogenic properties, and excellent strength and oxidation resistance up to 1300 F. It is highly recommended for missile and gas turbine components. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on low and high temperature performance, and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-112. Producer or source: Firth Sterling Inc..


Alloy Digest ◽  
1967 ◽  
Vol 16 (9) ◽  

Abstract Columbium WC-103 is a columbium-base alloy having good high temperature strength, good weldability and fabricability. It is recommended for high performance rocket engine components for temperatures up to 2800 F for controlled periods of time. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Cb-12. Producer or source: Wah Chang, a Teledyne Corporation.


Alloy Digest ◽  
1966 ◽  
Vol 15 (10) ◽  

Abstract COLUMBIUM-1% Zr is a readily fabricable, moderate strength columbium-base alloy for high temperature service. It is double consumable-electrode vacuum are melted. It is recommended for missiles, spacecraft and high temperature components. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness and creep. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Cb-11. Producer or source: Wah Chang.


Alloy Digest ◽  
1963 ◽  
Vol 12 (3) ◽  

Abstract COLUMBIUM D-31 is a columbium-base alloy that maintains its stability at very high temperatures. It is 5 times as resistant to oxidation as pure columbium and about 100 times as resistant as molybdenum. Its strength to density ratio at 2000 F (stress relieved) is 77400. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on high temperature performance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Cb-4. Producer or source: E. I. Dupont de Nemours & Company Inc..


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