Haynes Waspaloy is a specially vacuum melted, nickel-base alloy having outstanding tensile and stress-rupture strength up to 760 deg C (1400 deg F) combined with high oxidation resistance up to 871 deg C (1600 deg F). It is recommended for gas turbine engines, airframe assemblies, and missile systems. 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 heat treating and machining. Filing Code: Ni-560. Producer or source: Haynes International Inc.

AISI No. 651 is an austenitic iron-base superalloy with a relatively high ratio of strength to alloying element content. It is capable of withstanding high static and dynamic stresses through at least 1200 F. It is used for various high-temperature applications such as components for jet engines, gas turbines, turbochargers and missiles. This datasheet provides information on composition, physical properties, hardness, 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: SS-478. Producer or source: Stainless steel mills.

GUTERL H-11 is a 5% chromium hot-work tool steel with an excellent combination of red hardness, shock resistance (toughness) and resistance to abrasion; these are the properties needed for good hot-work characteristics. It will withstand drastic cooling from maximum operating temperatures. Among the many uses for this steel are hot-die applications, structural parts for jet engines and missiles, extrusion mandrels and forging dies. This datasheet provides information on composition, physical properties, hardness, and elasticity. It also includes information on forming, heat treating, machining, joining, and surface treatment. Filing Code: TS-412. Producer or source: Guterl Special Steel Corporation.

AISI No. 685 is a nickel-base, austenitic, precipitation-hardenable alloy. It has excellent tensile and stress-rupture strength to 1400 F and high resistance to corrosion and oxidation at temperatures at least to 1600 F. It is used widely in airframe assemblies, gas turbine engines and missile systems. This datasheet provides information on composition, physical properties, hardness, and tensile properties as well as fracture toughness and 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-271. Producer or source: Nickel alloy mills.

UDIMET 718 is a nickel-base alloy that is precipitation hardenable. It exhibits exceptionally high yield strength up to 1300 F, excellent cryogenic properties down to -423 F and superior weldability even in the fully-aged condition. This unusual combination of characteristics makes it suitable for elevated-temperature applications in gas turbines and in critical components for missiles. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-258. Producer or source: Special Metals Corporation.

ALUMINUM 356.0 is an aluminum casting alloy that normally is used only when heat-treated (aged) strengths are required. It is recommended for high strength, pressure-tight castings, intricate shapes and good resistance to corrosion. Its many applications include gear cases, instrument housings and components for aircraft and missiles. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness. It also includes information on high temperature performance and corrosion resistance as well as casting, heat treating, machining, and joining. Filing Code: Al-223. Producer or source: Various aluminum companies.

COLUMBIUM C-129Y is a columbium-tungsten-hafnium refractory alloy having good high temperature properties along with good heat and oxidation resistance. It is recommended for missiles, space craft and various high temperature applicatios. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep and fatigue. It also includes information on forming, heat treating, machining, and joining. Filing Code: Cb-16. Producer or source: Wah Chang, a Teledyne Corporation.

COLUMBIUM 10W-2.5Zr is a columbium-tungsten-zirconium alloy having good high temperature strength and heat resistance up to 2400 F. It is recommended for nuclear reactors, missiles and space vehicles. 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-15. Producer or source: Union Carbide Corporation, Stellite Division.

WASPALOY is a vacuum induction melted nickel-base alloy having outstanding tensil and stress-rupture strength up to 1400 F combined with high oxidation resistance up to 1600 F. It is recommended for gas turbine engines, airframe assemblies and missile systems. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness, creep, and fatigue. 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-129. Producer or source: Union Carbide Corporation, Materials Systems Division.

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.

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.

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.

HYLITE 20 is a titanium-aluminum-tin alloy with properties of medium tensile strength, good weldability and non-embrittlement under service conditions. It is recommended for aircraft and missile components. This datasheet provides information on composition, physical properties, 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, joining, and surface treatment. Filing Code: Ti-47. Producer or source: Jessop-Saville Ltd, Brightside Works.

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..

Magnesium-LA91 is a magnesium-lithium lightweight alloy recommended for missile and space vehicle structures. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as forming, machining, and joining. Filing Code: Mg-58. Producer or source: Brooks & Perkins Inc..

AISI No. 631 is chromium-nickel-aluminum precipitation hardening stainless steel recommended for aircraft, missile and jet engine parts. 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, joining, and surface treatment. Filing Code: SS-168. Producer or source: Alloy steel mills and foundries.

Pyromet 882 is an air-hardening 5% chromium tool steel recommended for high temperature applications up to 1000 F. It has extremely high tensile and creep strength. It is used for such critical applications as structural components in aircraft and missiles which require either extremely high strength (over 260,000 psi) at ambient temperature or high creep and rupture strength at temperatures of about 800 to 1200 F. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness, creep, and fatigue. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: TS-152. Producer or source: Carpenter Technology Corporation.

Magnesium-LA[4]A is a magnesium-lithium light weight alloy for missile and space vehicle structures. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and bearing strength as well as fracture toughness. It also includes information on low and high temperature performance, and corrosion resistance as well as casting, forming, heat treating, machining, and joining. Filing Code: Mg-56. Producer or source: Brooks & Perkins Inc..

Udimet B is a series of four 18%-nickel steels of ultra high strength and good toughness at room and at elevated temperatures. They are easily fabricated and weldable, and are recommended for the aircraft and missile industries for high temperature components. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: SA-146. Producer or source: Special Metals.

Crucible D6 is a low alloy ultra-high strength steel developed for aircraft-missile applications and primarily designed for use in the 260,000-290,000 psi tensile strength range. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness, creep, and fatigue. It also includes information on low temperature performance as well as forming, heat treating, machining, and joining. Filing Code: SA-129. Producer or source: Crucible Steel Company of America.