UNILOY 19-9DX is a chromium-nickel heat resistant super alloy, capable of withstanding high static and dynamic stresses through at least 1200 deg. F. It has very low strategic index. 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: SS-41. Producer or source: Cyclops Corporation.

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.

UNILOY 19-9DL is a chromium-nickel heat resistant super alloy, capable of withstanding high static and dynamic stresses through at least 1200 deg. 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 and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: SS-19. Producer or source: Cyclops Corporation.

Aluminum alloy 7449 in the T7651 temper is solution heat treated, stress relieved, and overaged. This processing produces an alloy of high strength, good corrosion/exfoliation resistance, and good toughness. An application of interest is the upper-wing skin of aircraft structures. This datasheet provides information on composition and tensile properties as well as fracture toughness. It also includes information on forming. Filing Code: AL-402. Producer or source: Pechiney Rolled Products LLC.

Kubota alloy KHR32C is often regarded as the cast version of Fe-Ni-Cr alloy 800H except it uses niobium as a strengthening agent. The moderately priced alloy has good creep ductility and is available in many cast forms. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on casting. Filing Code: SS-746. Producer or source: Kubota Metal Corporation.

Märker/Centralloy H101 is a Fe-Ni-Cr alloy matrix, designed to combine adequate strength with structural stability. Although originally designed to be a centrispun cast alloy, it is now available in static and investment cast product forms. This datasheet provides information on composition, physical properties, and tensile properties as well as creep. It also includes information on machining and joining. Filing Code: Ni-569. Producer or source: Schmidt & Clemens Inc.

Kubota Alloy KHR24C is an iron-nickel-chromium-niobium alloy with strength intermediate to HK 40 (Alloy Digest SS-303, December 1974) and HP alloys (Alloy Digest SS-307, March 1975). This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on casting and joining. Filing Code: SS-744. Producer or source: Kubota Metal Corporation.

Alcan 7056 is an Al-Mg-Zn-Cu-Zr alloy developed to provide an improved static/toughness balance versus incumbent 7150 and 7449 alloys. This data sheet covers Alcan 7056 alloy in the overaged T7951 temper. The alloy possesses very high toughness with improved corrosion resistance over 7150. This datasheet provides information on composition, physical properties, and tensile properties as well as fracture toughness. It also includes information on corrosion resistance as well as forming and heat treating. Filing Code: AL-416. Producer or source: Alcan Inc.

Kubota alloy KHR12C is an austenitic Fe-Cr-Ni-Nb casting alloy developed from the well known HH type II grade. This alloy is superior to other grades in components that are subjected to frequent thermal cycling and shock. The alloy is available in both centrifugal and static castings. This datasheet provides information on composition, physical properties, and tensile properties as well as creep. It also includes information on high temperature performance as well as casting and joining. Filing Code: SS-738. Producer or source: Kubota Metal Corporation.

IN-519 was developed primarily for application as centrifugally cast tubes in steam-hydrocarbon reformer furnaces. It has significantly higher stress-rupture properties than HK-40 (25Cr-20Ni), which is most commonly used for such 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 casting, heat treating, machining, and joining. Filing Code: SS-246. Producer or source: Abex Corporation, Engineered Products Division.

KHRS2 is a Fe-Cr-Ni-Co alloy with tungsten. The alloy was developed for high-temperature service such as radiant heater tubes. This datasheet provides information on composition, physical properties, and tensile properties as well as creep. It also includes information on high temperature performance as well as joining. Filing Code: SS-858. Producer or source: Kubota Metal Corporation, Fahramet Division.

PRECEDENT-71 is an aluminum casting alloy that age hardens at room temperature. It is recommended for heavy shock and high static loads, and for severe fatigue and endurance loading. The alloy is supplied in two grades. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as casting, heat treating, machining, and joining. Filing Code: Al-113. Producer or source: William F. Jobbins Inc..

Alcan 2098 and 2x98 are Al-Cu-Li-Mg-Ag alloys designed to provide a balanced combination of high strength, low density, fatigue resistance, and fracture toughness for aerospace applications. This data sheet covers Alcan 2098 and 2x98 Al-Li fuselage sheets. The O and T82P tempers show improvement over the 2024 alloy. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on corrosion resistance as well as forming and heat treating. Filing Code: AL-405. Producer or source: Alcan Inc.

KHRS3 is a Ni-Cr-Fe-Co-W alloy developed for greater strength in high-temperature service such as in radiant heater tubes. This datasheet provides information on composition, physical properties, and tensile properties as well as creep. It also includes information on high temperature performance and corrosion resistance as well as joining. Filing Code: Ni-598. Producer or source: Kubota Metal Corporation, Fahramet Division.

AA 771.0 is an aluminum casting alloy that age hardens at room temperature. It also may be age hardened by a number of temper heat treatments. It is recommended for heavy shock and high static loads, and also for severe fatigue loading. Its uses include aircraft guidance systems and computing devices. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on casting, heat treating, machining, and joining. Filing Code: Al-283. Producer or source: Various aluminum companies.

Kubota KHR35W has additions of tungsten to 25Cr-35Ni base alloy (Alloy digest SS-755, August 1999). The tungsten is used to further increase carburization resistance in service at temperatures up to 1095 C (2000 F). This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep. It also includes information on corrosion resistance as well as joining. Filing Code: Ni-573. Producer or source: Kubota Metal Corporation.

KHR35H is a high-temperature heat resistant alloy with a molybdenum addition to increase creep and rupture strength to levels better than those of HP alloy. Typical applications are in heat treatment equipment. This datasheet provides information on composition, physical properties, and tensile properties as well as creep. It also includes information on corrosion resistance as well as joining. Filing Code: Ni-564. Producer or source: Kubota Metal Corporation.

KHR35H-HiSi is an improvement over HP alloy in oxidation resistance and creep strength. This composition also has high silicon for resisting carburizing environments in ethylene pyrolysis coils. This datasheet provides information on composition, physical properties, and tensile properties as well as creep. It also includes information on corrosion resistance. Filing Code: Ni-567. Producer or source: Kubota Metal Corporation.

INCOLOY alloy 903 is a precipitation hardenable nickel-iron-cobalt alloy whose outstanding characteristics are a constant low coefficient of thermal expansion, a constant modulus of elasticity and high strength. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Fe-50. Producer or source: Huntington Alloy Products Division, An INCO Company.

Centralloy G4852 Micro R is a cast austenitic stainless steel with very good high temperature properties. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on casting, machining, and joining. Filing Code: SS-1137. Producer or source: Schmidt & Clemens Inc..