COLUMBIUM SCB-291

Alloy Digest ◽  
1968 ◽  
Vol 17 (1) ◽  
Keyword(s):  
High Temperature ◽  
Physical Properties ◽  
Tensile Properties ◽  
Nuclear Reactors ◽  
Base Alloy ◽  
Heat Treating ◽  
Space Vehicles ◽  
High Temperature Properties ◽  
Chemical Company ◽  
Temperature Performance

Abstract Columbium SCB-291 is a columbium-base alloy having excellent high temperature properties and good fabricability. It is recommended for nuclear reactors, space vehicles, jet and missile components. This datasheet provides information on composition, physical properties, hardness, and tensile properties as well as creep. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Cb-14. Producer or source: Stauffer Metals Division, Stauffer Chemical Company.

HAYNES ALLOY No. Cb-752

Alloy Digest ◽  
1963 ◽  
Vol 12 (11) ◽  
Keyword(s):  
High Temperature ◽  
Physical Properties ◽  
Tensile Properties ◽  
Nuclear Reactors ◽  
Base Alloy ◽  
Heat Treating ◽  
Space Vehicles ◽  
Union Carbide Corporation ◽  
Temperature Performance ◽  
Haynes Alloy

Abstract HAYNES Alloy Cb-752 is a columbium-base alloy having good high temperature characteristics. It has 25,000 psi ultimate strength at 2400 F. It is recommended for space vehicles and nuclear reactors. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear andbearing strength as well as creep. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Cb-6. Producer or source: Union Carbide Corporation, Stellite Division.

COLUMBIUM 10W-10Hf

Alloy Digest ◽  
1967 ◽  
Vol 16 (10) ◽  
Keyword(s):  
High Temperature ◽  
Physical Properties ◽  
Tensile Properties ◽  
Oxidation Resistance ◽  
Base Alloy ◽  
Heat Treating ◽  
Space Vehicles ◽  
Bend Strength ◽  
Good Oxidation Resistance ◽  
Temperature Performance

Abstract COLUMBIUM-10W-10Hf is a columbium-base alloy having good oxidation resistance and good high temperature properties. It is recommended for high temperature applications such as missiles, space vehicles, etc. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and bend strength as well as creep. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Cb-13. Producer or source: Wah Chang, a Teledyne Corporation.

MAGNESIUM HM31A

Alloy Digest ◽  
1966 ◽  
Vol 15 (5) ◽  
Keyword(s):  
Corrosion Resistance ◽  
High Temperature ◽  
Elevated Temperature ◽  
Physical Properties ◽  
Tensile Properties ◽  
Heat Treating ◽  
Space Vehicles ◽  
Bearing Strength ◽  
Chemical Company ◽  
Temperature Performance

Abstract Magnesium HM331A is a magnesium-thorium alloy recommended for elevated temperature service (600-850 F) in aircraft, missiles, and space vehicles. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive, shear, and bearing strength as well as creep and fatigue. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Mg-59. Producer or source: Dow Chemical Company.

MAGNESIUM HZ32A

Alloy Digest ◽  
1959 ◽  
Vol 8 (6) ◽  
Keyword(s):  
Corrosion Resistance ◽  
High Temperature ◽  
Elevated Temperature ◽  
Physical Properties ◽  
Tensile Properties ◽  
Base Alloy ◽  
Heat Treating ◽  
Chemical Company ◽  
Temperature Performance ◽  
Temperature Applications

Abstract MAGNESIUM HZ 32A is a magnesium-base alloy containing thorium, zirconium and zinc. It is recommended for elevated temperature 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 and corrosion resistance as well as casting, heat treating, machining, and joining. Filing Code: Mg-42. Producer or source: Dow Chemical Company, Magnesium Department.

MAR-M Alloy 200

Alloy Digest ◽  
1965 ◽  
Vol 14 (11) ◽  
Keyword(s):  
High Temperature ◽  
Physical Properties ◽  
Tensile Properties ◽  
Turbine Blade ◽  
Base Alloy ◽  
Heat Treating ◽  
Nickel Base Alloy ◽  
Temperature Performance ◽  
Nickel Base

Abstract MAR-M Alloy 200 is a nickel-base alloy designed primarily as a cast turbine blade material which retains useful strength up to 1900 F. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on high temperature performance as well as heat treating and joining. Filing Code: Ni-107. Producer or source: Martin Metals Company.

FLYLITE ZRE-1

Alloy Digest ◽  
1952 ◽  
Vol 1 (2) ◽  
Keyword(s):  
Compressive Strength ◽  
High Temperature ◽  
Physical Properties ◽  
Tensile Properties ◽  
Base Alloy ◽  
Heat Treating ◽  
Jet Engine ◽  
Temperature Performance ◽  
Engine Components ◽  
Temperature Applications

Abstract Flylite ZRE-1 is a creep resistant magnesium-base alloy primarily designed for jet engine components and other high temperature applications. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive strength as well as creep. It also includes information on high temperature performance as well as casting, heat treating, machining, and joining. Filing Code: Mg-2. Producer or source: Howard Foundry Company.

COLUMBIUM 15W-5Mo-1Zr

Alloy Digest ◽  
1969 ◽  
Vol 18 (12) ◽  
Keyword(s):  
High Temperature ◽  
Physical Properties ◽  
Tensile Properties ◽  
Structural Properties ◽  
Base Alloy ◽  
Heat Treating ◽  
Temperature Performance

Abstract Columbium 15W-5 Mo- 1Zr is a columbium-base alloy capable of retaining usuable structural properties up to 2500 F. 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, and joining. Filing Code: Cb-17. Producer or source: Fansteel Metallurgical Corporation.

MAGNESIUM ZK60A

Alloy Digest ◽  
1967 ◽  
Vol 16 (4) ◽  
Keyword(s):  
Fracture Toughness ◽  
Corrosion Resistance ◽  
High Temperature ◽  
Physical Properties ◽  
Tensile Properties ◽  
High Strength ◽  
Heat Treating ◽  
Bend Strength ◽  
Chemical Company ◽  
Temperature Performance

Abstract Magnesium ZK60A is a heat treatable extrusion and forging alloy recommended for applications where high strength with good toughness are required. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and compressive, shear, bearing, and bend strength as well as fracture toughness. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Mg-62. Producer or source: The Dow Chemical Company.

MAGNESIUM AZ61A

Alloy Digest ◽  
1959 ◽  
Vol 8 (8) ◽  
Keyword(s):  
Corrosion Resistance ◽  
High Temperature ◽  
Physical Properties ◽  
Surface Treatment ◽  
Tensile Properties ◽  
Heat Treating ◽  
Bearing Strength ◽  
Chemical Company ◽  
Temperature Performance ◽  
Extrusion Alloy

Abstract MAGNESIUM AZ61A is a magnesium extrusion alloy having a strength level between that of AZ31B and ZK60A. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive, shear, and bearing strength as well as fatigue. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Mg-43. Producer or source: The Dow Chemical Company.

NICKELVAC L-605

Alloy Digest ◽  
1967 ◽  
Vol 16 (10) ◽  
Keyword(s):  
Corrosion Resistance ◽  
High Temperature ◽  
Physical Properties ◽  
Tensile Properties ◽  
Base Alloy ◽  
Heat Treating ◽  
Temperature Range ◽  
Temperature Performance ◽  
Cobalt Base Alloy ◽  
Cobalt Base

Abstract NICKELVAC L-605 is a double vacuum melted, cobalt-base alloy for high temperature applications. It is recommended for highly stressed parts operating in the temperature range of 1700 to 2000 F. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as creep and fatigue. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Co-53. Producer or source: Allvac Metals Company, A Teledyne Company.

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