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aircraft-missile applications
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Journal Articles
Publisher: Journals Gateway
Alloy Digest (1962) 11 (5): SA-129.
Published: 01 May 1962
... 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...
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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.
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Publisher: Journals Gateway
Alloy Digest (1964) 13 (10): TS-152.
Published: 01 October 1964
... 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...
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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.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1979) 28 (4): Al-234.
Published: 01 April 1979
... impact values, (2) The best combination of room and elevated-temperature performance, and (3) The best ballistic properties. Its ballistic properties are comparable to those of the standard wrought aluminum aBoys Among its many applications are com- ponents for military aircraft and missiles...
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ALUMINUM A201 offers high strength, high impact resistance, a good combination of room and elevated-temperature performance, and good ballistic properties. Its ballistic properties are comparable to those of the standard wrought aluminum alloys. Among its many application are components for military aircraft and missiles, and impellers for gas turbine engines. This datasheet provides information on composition, physical properties, 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 casting, heat treating, machining, joining, and surface treatment. Filing Code: Al-234. Producer or source: Consolidated Aluminum Corporation.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1976) 25 (5): Al-223.
Published: 01 May 1976
... shapes and good resistance to corrosion. Its many applications include gear cases, instru- ment housings and components for aircraft and missiles. Composition: Physical Constants: Silicon 6.5-7.5 Density, lb/cu in. 0.097 Iron 0.6 max. Specific gravity 2.68 Copper 0.25 max. Melting range, oF Manganese...
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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.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1960) 9 (4): Mg-46.
Published: 01 April 1960
... MAGNESIUM HM21A is a magnesium alloy sheet, plate, and forging material developed for high temperature service as in aircraft and missile applications. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and bearing...
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MAGNESIUM HM21A is a magnesium alloy sheet, plate, and forging material developed for high temperature service as in aircraft and missile applications. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and bearing strength 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: Mg-46. Producer or source: The Dow Metal Products Company.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1969) 18 (7): Al-188.
Published: 01 July 1969
... ALUMINUM 359 is a high strength, corrosion resistant aluminum casting alloy recommended for aircraft and missile applications. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear strength. It also includes...
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ALUMINUM 359 is a high strength, corrosion resistant aluminum casting alloy recommended for aircraft and missile applications. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear strength. It also includes information on low and high temperature performance, and corrosion resistance as well as casting, heat treating, machining, and joining. Filing Code: Al-188. Producer or source: Aluminum Company of America.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1969) 18 (11): SS-231.
Published: 01 November 1969
... can be heat treated to the highest hardness and strength level. It is recommended for many applications where corrosion and osida:ion resistance coupled with high strength and wear resistance are required as in bearings. cams and rollers in aircraft and missile fields. Composition: Carbon Manganese...
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AISI No. 617 is a general purpose hardenable stainless steel which can be heat treated to the highest hardness and strength level. It is recommended for many applications where corrosion and oxidation resistance coupled with high strength and wear resistance are required as in bearings, cams and rollers in aircraft and missile fields. This datasheet provides information on composition, physical properties, microstructure, hardness, elasticity, tensile properties, and compressive strength as well as fracture toughness. 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-231. Producer or source: Stainless steel mills.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1970) 19 (2): SS-234.
Published: 01 February 1970
... ALLEGHENY ALMAR-362 is an age-hardenable martensitic stainless steel recommended for applications requiring high strength and good corrosion resistance, such as aircraft and missile structures, hydraulic and pneumatic equipment components, and in the chemical processing industry. This datasheet...
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ALLEGHENY ALMAR-362 is an age-hardenable martensitic stainless steel recommended for applications requiring high strength and good corrosion resistance, such as aircraft and missile structures, hydraulic and pneumatic equipment components, and in the chemical processing industry. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive strength as well as fracture toughness. It also includes information on corrosion resistance as well as casting, forming, heat treating, machining, joining, and surface treatment. Filing Code: SS-234. Producer or source: Allegheny Ludlum Corporation.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1963) 12 (5): SA-146.
Published: 01 May 1963
... is maintained ar 6000F. It is a vacuum induction melted steel designed co achieve a yield stress in excess of 300,000 psi. Forms Available: Billets, bars, sheet, strip and wire. Applications: Aircraft and rocket engines, airframe and missile systems. Manufacturer: Special Metals, Inc. New Hartford, New York...
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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.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1982) 31 (5): Al-238.
Published: 01 May 1982
... further by anodizing. It has excellent welding characteristics. Forms Available: Sand and permanent-mold castings. Applications: Typical uses of Aluminum 357.0 are aircraft, missile and aerospace components and other items that need heat-treatable castings that combine excellent weld- ability, high...
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ALUMINUM 357.0 is a high-purity aluminum casting alloy that can be solution treated and aged to develop high tensile and yield strengths along with fairly good ductility. Among its uses are aircraft, missile and aerospace components and cylinder blocks for water-cooled engines. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on corrosion resistance as well as casting, heat treating, machining, and joining. Filing Code: Al-238. Producer or source: Various aluminum companies.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1966) 15 (5): Mg-59.
Published: 01 May 1966
.... The minimum burning temper- ature is above 900oF. Its recrystallization temperature is 7500F for one hour after 50% cold work. Forms Available: Extrusions, extruded bars and rods, shapes and cubing. Applications: High temperature (600-85OoF) aircraft service, missile components. Manufacturer: Dow Chemical...
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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.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1969) 18 (11): Al-192.
Published: 01 November 1969
... Aluminum A356 is a sand and permanent mold casting alloy that responds to an age-hardening heat treatment. It is recommended for aircraft and missile components where high strength and corrosion resistance are required. This datasheet provides information on composition, physical properties...
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Aluminum A356 is a sand and permanent mold casting alloy that responds to an age-hardening heat treatment. It is recommended for aircraft and missile components where high strength and corrosion resistance are required. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear strength as well as fatigue. It also includes information on heat treating, machining, and joining. Filing Code: Al-192. Producer or source: Aluminum Company of America.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1967) 16 (6): Mg-63.
Published: 01 June 1967
.... Forms Available: Sand castings, Applications: Transmission cases, missile components, aircraft nose wheels, rockets, racing auromobile pistons, components of hydraulic units. Manufacturer: J. Stone 8~ Co. (Charlron) Ltd. London, England Magnesium Elektron Lrd. Manchester, England ...
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Magnesium MSR-B is a heat-treatable magnesium alloy with highest yield strength of any cast magnesium alloy up to 480 F. It is pressure tight and weldable by argon-arc. It is recommended for aircraft nose wheels, missile components, transmission cases, etc. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and shear strength as well as fatigue. It also includes information on low and high temperature performance, and corrosion resistance as well as casting, heat treating, machining, and joining. Filing Code: Mg-63. Producer or source: Magnesium Elektron Ltd.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1966) 15 (4): Ti-47.
Published: 01 April 1966
... or stress-relieved condition). Applications: Aircraft and missile components, compressor discs and cases, fasteners, wheel components, agitators, rank linings, bulk heads,pump housings,anodizing equipment. Manufacturer: Jessopdaville Ltd. Sheffield, England ...
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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.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1969) 18 (6): Al-187.
Published: 01 June 1969
... Aluminum A-140 is a non-heat treatable casting alloy having high tensile and fatigue strength at elevated temperatures to 600 F. It is recommended for engine cylinder heads, aircraft and missile components. This datasheet provides information on composition, physical properties, hardness...
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Aluminum A-140 is a non-heat treatable casting alloy having high tensile and fatigue strength at elevated temperatures to 600 F. It is recommended for engine cylinder heads, aircraft and missile components. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive strength. It also includes information on high temperature performance as well as casting, heat treating, machining, and joining. Filing Code: Al-187. Producer or source: Aluminum Company of America.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1967) 16 (5): SA-209.
Published: 01 May 1967
.... Forms Available: Billets, bars, rod, forgings, plates and wire. Applications: Rocket motor cases, ship plate, pressure vessels, aircraft landing gears, missiles and aircraft engine components. Manufacturer: Republic Steel Corporation Massilloo, Ohio ...
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Republic RSM-200 is a high strength, tough maraging steel recommended for airframe and missile systems. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness and fatigue. It also includes information on corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: SA-209. Producer or source: Republic Steel Corporation.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1987) 36 (12): TS-487.
Published: 01 December 1987
... toughness. MOLITE is especially recommended for tools used in the machining of high-strength steels, prehardened steels and exotic ferrous and nonferrous alloys such as are used in aircraft and missile work. It is also recommended for ordinary machining jobs requiring long production runs. This datasheet...
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MOLITE 42 is a molybdenum-type super high-speed steel. It has a well-balanced composition designed to give superior performance when used for difficult machining operations. It can be heat treated to a hardness level of Rockwell C 68-70 giving excellent red hardness while maintaining moderate toughness. MOLITE is especially recommended for tools used in the machining of high-strength steels, prehardened steels and exotic ferrous and nonferrous alloys such as are used in aircraft and missile work. It is also recommended for ordinary machining jobs requiring long production runs. This datasheet provides information on composition, physical properties, hardness, and elasticity. It also includes information on forming, heat treating, and machining. Filing Code: TS-487. Producer or source: Columbia Tool Steel Company.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1965) 14 (5): SS-168.
Published: 01 May 1965
... of the American Iron and Steel Institute entitled High Temperature High Screngch Alloys Forms Available: Sheet, scrip, place, wire, angles, bars, and forging billers. Applications: Aircraft skins and structural members, missile pressure tanks and structural members, jet engine parts, helical and flat springs...
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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.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1968) 17 (4): SA-225.
Published: 01 April 1968
... and fasteners. aircraft structural components, aircraft landing gear, missile and aircraft engine com- ponents, pressure vessels, extrusion mandrels, die bolsters and other tooling applications. Manufacturer: Jessop-Saville Ltd. Sheffield, England ...
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G.110 is an 18% nickel alloy steel, possessing an excellent combination of toughness and ductility at yield strength levels of 250,000 psi. The strength developed is independent of mass effect and rate of cooling, and is achieved by a simple aging treatment. The alloy is recommended for applications such as rocket motor cases and accessories, bolts and fasteners and aircraft structural components- particularly landing gear. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness. It also includes information on forming, heat treating, joining, and surface treatment. Filing Code: SA-225. Producer or source: Jessop-Saville Ltd, Brightside Works.
Journal Articles
Publisher: Journals Gateway
Alloy Digest (1962) 11 (11): Al-120.
Published: 01 November 1962
.... Spec.) General Characteristics: Impalco 770 is a heat treatable aluminum alloy recommended for applications where very good strength and moderate resistance to cor- rosion are required. It is used primarily in aircraft and missile structural parts. In general, strengths and elongations are un- changed...
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IMPALCO 770 is a heat treatable, high strength aluminum alloy available in bar form for machining applications. It is recommended for highly stressed structural parts. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength as well as fracture toughness and fatigue. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Al-120. Producer or source: Imperial Aluminium Company Ltd.