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Journal Articles
Alloy Digest (1984) 33 (7): TS-425.
Published: 01 July 1984
... VascoJet 2000 was developed to meet the needs of the aerospace industry. It also has been used for special tooling applications. It is a vacuum-melted modification of AISI H12 hot-work die steel. VascoJet 2000 has a tensile strength of 200,000 psi (1500 MPa) at room temperature and exceptional...
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View articletitled, VASCOJET 2000: Tool Steel for Carburizing
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for article titled, VASCOJET 2000: Tool Steel for Carburizing
VascoJet 2000 was developed to meet the needs of the aerospace industry. It also has been used for special tooling applications. It is a vacuum-melted modification of AISI H12 hot-work die steel. VascoJet 2000 has a tensile strength of 200,000 psi (1500 MPa) at room temperature and exceptional toughness. It is used for gears and shafts in helicopter and other aerospace applications. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on high temperature performance as well as forming, heat treating, machining, and joining. Filing Code: TS-425. Producer or source: Teledyne Vasco.
Journal Articles
Alloy Digest (2009) 58 (6): Al-422.
Published: 01 June 2009
... ALCOA 2099 is an aluminum-lithium alloy developed for aerospace applications. Lithium lowers the density. This datasheet provides information on composition, physical properties, tensile properties, and compressive strength as well as fatigue. It also includes information on corrosion resistance...
Abstract
View articletitled, ALCOA 2099-T83 and 2099-T8E67: Aluminum Extrusion Alloy
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for article titled, ALCOA 2099-T83 and 2099-T8E67: Aluminum Extrusion Alloy
ALCOA 2099 is an aluminum-lithium alloy developed for aerospace applications. Lithium lowers the density. This datasheet provides information on composition, physical properties, tensile properties, and compressive strength as well as fatigue. It also includes information on corrosion resistance as well as forming. Filing Code: AL-422. Producer or source: AEAP-Alcoa Engineered Aerospace Products.
Journal Articles
Alloy Digest (1983) 32 (4): Ni-285.
Published: 01 April 1983
.... It is outstanding in resistance to corrosion either general or localized (pitting/crevice), is virtually immune to chloride-ionstress-corrosion cracking, and is highly resistant to oxidation. Among its many uses are aerospace applications, heat exchangers, nuclear-reactor components and power-plant flue-gas...
Abstract
View articletitled, JESSOP JS625: High Temperature Alloy
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for article titled, JESSOP JS625: High Temperature Alloy
JESSOP JS625 is a nickel-chromium-molybdenum-columbium alloy that is well suited for applications where strength and corrosion resistance are required. It has superior strength and toughness at temperatures ranging from cryogenic to 2000 F; also, it has exceptional fatigue strength. It is outstanding in resistance to corrosion either general or localized (pitting/crevice), is virtually immune to chloride-ionstress-corrosion cracking, and is highly resistant to oxidation. Among its many uses are aerospace applications, heat exchangers, nuclear-reactor components and power-plant flue-gas scrubbers. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: Ni-285. Producer or source: Jessop Steel Company.
Journal Articles
Alloy Digest (1983) 32 (10): Fe-69.
Published: 01 October 1983
... aerospace applications where small core size is a requirement, and to pulse applications where maximum flux swing is desired. This datasheet provides information on composition and physical properties. It also includes information on forming and heat treating. Filing Code: Fe-69. Producer or source: Allied...
Abstract
View articletitled, METGLAS ALLOY 2605CO: Amorphous Soft Magnetic Alloy
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for article titled, METGLAS ALLOY 2605CO: Amorphous Soft Magnetic Alloy
METGLAS Alloy 2605CO is an amorphous iron-base soft magnetic alloy. It has the highest saturation induction of any amorphous alloy commercially available, combined with very low core loss. It is the alloy of choice when low weight is as important as efficiency. It is particularly suited to 400 Hz aerospace applications where small core size is a requirement, and to pulse applications where maximum flux swing is desired. This datasheet provides information on composition and physical properties. It also includes information on forming and heat treating. Filing Code: Fe-69. Producer or source: Allied Corporation, Metglass Products Department.
Journal Articles
Alloy Digest (1974) 23 (11): Al-210.
Published: 01 November 1974
... FEDERATED F410 is a heat-treatable aluminum sand casting alloy recommended for uses requiring high strength along with toughness and ductility. It has good machinability, fair castability, and is suitable for a number of automotive and aerospace applications. This datasheet provides information...
Abstract
View articletitled, FEDERATED F410: Heat Treatable Aluminum Casting Alloy
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for article titled, FEDERATED F410: Heat Treatable Aluminum Casting Alloy
FEDERATED F410 is a heat-treatable aluminum sand casting alloy recommended for uses requiring high strength along with toughness and ductility. It has good machinability, fair castability, and is suitable for a number of automotive and aerospace applications. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness. It also includes information on corrosion resistance as well as casting, heat treating, machining, and joining. Filing Code: Al-210. Producer or source: Federated Metals Corporation, ASARCO Inc..
Journal Articles
Alloy Digest (2004) 53 (8): Cu-722.
Published: 01 August 2004
... BrushBronze 95510 is an aluminum nickel bronze alloy that combines high strength, ductility, and good abrasion resistance under severe loading conditions. This material, specified as AMS 4880, is frequently used for very demanding aerospace applications. This datasheet provides information...
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View articletitled, BRUSHBRONZE 95510: Aluminum Nickel Bronze
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for article titled, BRUSHBRONZE 95510: Aluminum Nickel Bronze
BrushBronze 95510 is an aluminum nickel bronze alloy that combines high strength, ductility, and good abrasion resistance under severe loading conditions. This material, specified as AMS 4880, is frequently used for very demanding aerospace applications. This datasheet provides information on composition, microstructure, and tensile properties. Filing Code: CU-722. Producer or source: Brush Wellman Inc.
Journal Articles
Alloy Digest (2007) 56 (8): Al-405.
Published: 01 August 2007
... 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...
Abstract
View articletitled, ALCAN 2098, 2X98 O/T82P: Aluminum-Lithium Alloy Fuselage Sheets
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for article titled, ALCAN 2098, 2X98 O/T82P: Aluminum-Lithium Alloy Fuselage Sheets
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.
Journal Articles
Alloy Digest (2007) 56 (10): Al-406.
Published: 01 October 2007
... Alcan 7449 T7651 plates were developed with a better strength/corrosion-resistance balance than the incumbent alloy 7150. Aerospace applications include parts, ribs, and frames. This datasheet provides information on composition, physical properties, and tensile properties as well as fracture...
Abstract
View articletitled, ALCAN 7449 T7651: Aluminum <span class="search-highlight">Aerospace</span> Plate
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for article titled, ALCAN 7449 T7651: Aluminum <span class="search-highlight">Aerospace</span> Plate
Alcan 7449 T7651 plates were developed with a better strength/corrosion-resistance balance than the incumbent alloy 7150. Aerospace applications include parts, ribs, and frames. This datasheet provides information on composition, physical properties, and tensile properties as well as fracture toughness and fatigue. It also includes information on forming and heat treating. Filing Code: AL-406. Producer or source: Alcan Inc.
Journal Articles
Alloy Digest (2007) 56 (11): Al-407.
Published: 01 November 2007
... Alcan 7449 T7951 plates were developed with a better strength/corrosion-resistance balance over the incumbent alloy 7150. This temper produces better age-forming capability. Aerospace applications include parts, ribs, and frames. This datasheet provides information on composition, tensile...
Abstract
View articletitled, ALCAN 7449 T7951: Aluminum <span class="search-highlight">Aerospace</span> Plate
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for article titled, ALCAN 7449 T7951: Aluminum <span class="search-highlight">Aerospace</span> Plate
Alcan 7449 T7951 plates were developed with a better strength/corrosion-resistance balance over the incumbent alloy 7150. This temper produces better age-forming capability. Aerospace applications include parts, ribs, and frames. This datasheet provides information on composition, tensile properties, and compressive strength as well as fracture toughness. It also includes information on corrosion resistance as well as forming and heat treating. Filing Code: AL-407. Producer or source: Alcan Inc.
Journal Articles
Alloy Digest (2007) 56 (12): Al-408.
Published: 01 December 2007
... Alcan 6156 T4, T6 clad sheets were developed with weldability and high damage tolerance compared with incumbent 2024 alloy. Aerospace applications include fuselages clad sheets. This datasheet provides information on composition, physical properties, and tensile properties as well as fatigue...
Abstract
View articletitled, ALCAN 6156 T4, T62: Aluminum Fuselage Clad Sheets
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for article titled, ALCAN 6156 T4, T62: Aluminum Fuselage Clad Sheets
Alcan 6156 T4, T6 clad sheets were developed with weldability and high damage tolerance compared with incumbent 2024 alloy. Aerospace applications include fuselages clad sheets. This datasheet provides information on composition, physical properties, and tensile properties as well as fatigue. It also includes information on forming, heat treating, and joining. Filing Code: AL-408. Producer or source: Alcan Inc.
Journal Articles
Alloy Digest (2008) 57 (2): Al-410.
Published: 01 February 2008
... Alcan 2195 T8R78 is an addition to the Weldalite Al-Cu-Li-Ag-Mg-Zr family of alloys. It is a highly damage tolerant weldable alloy for aerospace applications. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness...
Abstract
View articletitled, ALCAN 2195 T8R78: Aluminum-Lithium Plates
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for article titled, ALCAN 2195 T8R78: Aluminum-Lithium Plates
Alcan 2195 T8R78 is an addition to the Weldalite Al-Cu-Li-Ag-Mg-Zr family of alloys. It is a highly damage tolerant weldable alloy for aerospace applications. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness. It also includes information on low temperature performance and corrosion resistance as well as forming, heat treating, and machining. Filing Code: AL-410. Producer or source: Alcan Inc.
Journal Articles
Alloy Digest (2016) 65 (6): SS-1247.
Published: 01 June 2016
... UGI 4057 Air is a carbon martensitic stainless steel with nickel for aerospace applications. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness. It also includes information on corrosion resistance...
Abstract
View articletitled, UGI 4057 AIR: Machinable Grade Austenitic Stainless Steel
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for article titled, UGI 4057 AIR: Machinable Grade Austenitic Stainless Steel
UGI 4057 Air is a carbon martensitic stainless steel with nickel for aerospace applications. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness. It also includes information on corrosion resistance as well as forming, heat treating, and joining. Filing Code: SS-1247. Producer or source: Schmolz + Bickenbach USA Inc..
Journal Articles
Alloy Digest (2018) 67 (2): SS-1280.
Published: 01 February 2018
... UGI 4545 Air is a precipitation hardening martensitic stainless steel designed for aerospace applications. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as forming...
Abstract
View articletitled, UGI 4545 AIR: Precipitation Hardening Martensitic Stainless Steel
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for article titled, UGI 4545 AIR: Precipitation Hardening Martensitic Stainless Steel
UGI 4545 Air is a precipitation hardening martensitic stainless steel designed for aerospace applications. 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, and joining. Filing Code: SS-1280. Producer or source: Schmolz + Bickenbach USA Inc..
Journal Articles
Alloy Digest (1978) 27 (10): SS-356.
Published: 01 October 1978
... Remelted) to consistently assure good cleanliness and superior properties. It is used for bearings, gears, ball screws and other aerospace applications. This datasheet provides information on composition, physical properties, hardness, and elasticity as well as fatigue. It also includes information...
Abstract
View articletitled, LESCALLOY BG42 VIM-VAR: Martensitic, Stainless, High-Speed Steel
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for article titled, LESCALLOY BG42 VIM-VAR: Martensitic, Stainless, High-Speed Steel
LESCALLOY BG42 VIM-VAR combines the tempering, hardness and hardness-retention characteristics of AISI M50 high-speed steel with the corrosion and oxidation resistance of AISI Type 440C stainless steel. LESCALLOY BG42 VIM-VAR is double vacuum melted (VIM, Vacuum Induction Melted; VAR, Vacuum Arc Remelted) to consistently assure good cleanliness and superior properties. It is used for bearings, gears, ball screws and other aerospace applications. This datasheet provides information on composition, physical properties, hardness, and elasticity as well as fatigue. It also includes information on corrosion and wear resistance as well as forming, heat treating, machining, and joining. Filing Code: SS-356. Producer or source: Latrobe Steel Company. See also Alloy Digest SS-179, revised February 1992.
Journal Articles
Alloy Digest (1967) 16 (2): Ni-121.
Published: 01 February 1967
... INCONEL alloy 625 is a nickel-base alloy having excellent stress-rupture properties and good oxidation resistance to 1200 F. It is recommended for jet engine components, aerospace applications and chemical processing equipment. This datasheet provides information on composition, physical...
Abstract
View articletitled, INCONEL ALLOY 625: High Temperature Alloy
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for article titled, INCONEL ALLOY 625: High Temperature Alloy
INCONEL alloy 625 is a nickel-base alloy having excellent stress-rupture properties and good oxidation resistance to 1200 F. It is recommended for jet engine components, aerospace applications and chemical processing equipment. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness. It also includes information on low temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ni-121. Producer or source: Huntington Alloy Products Division, An INCO Company.
Journal Articles
Alloy Digest (1993) 42 (12): Ni-443.
Published: 01 December 1993
... ALTEMP 625 is an austenitic nickel-base superalloy possessing excellent resistance to oxidation and corrosion over a broad range of corrosive conditions. The alloy is frequently used in aerospace applications as well as in the chemical process industry. This datasheet provides information...
Abstract
View articletitled, ALTEMP 625: Nickel-Base Superalloy
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for article titled, ALTEMP 625: Nickel-Base Superalloy
ALTEMP 625 is an austenitic nickel-base superalloy possessing excellent resistance to oxidation and corrosion over a broad range of corrosive conditions. The alloy is frequently used in aerospace applications as well as in the chemical process industry. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on high temperature performance as well as forming, heat treating, and joining. Filing Code: Ni-443. Producer or source: Allegheny Ludlum Corporation.
Journal Articles
Alloy Digest (1994) 43 (4): Fe-107.
Published: 01 April 1994
... AerMet 100 alloy possesses a combination of high strength, hardness, toughness and good resistance to stress-corrosion from chlorides. It can be used for many aerospace applications such as landing gear and fasteners. This datasheet provides information on composition, physical properties...
Abstract
View articletitled, AERMET 100 ALLOY: High Hardness High-Strength Alloy
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for article titled, AERMET 100 ALLOY: High Hardness High-Strength Alloy
AerMet 100 alloy possesses a combination of high strength, hardness, toughness and good resistance to stress-corrosion from chlorides. It can be used for many aerospace applications such as landing gear and fasteners. 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 heat treating. Filing Code: FE-107. Producer or source: Carpenter.
Journal Articles
Alloy Digest (1997) 46 (6): Co-103.
Published: 01 June 1997
... Conicro 5010W has a face-centered cubic structure and is a cobalt-base alloy containing chromium, tungsten, and nickel. The alloy is used in aerospace applications and in the heat-treatment industry. This datasheet provides information on composition, physical properties, and elasticity. It also...
Abstract
View articletitled, CONICRO 5010W: High-Temperature Cobalt-Base Alloy
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for article titled, CONICRO 5010W: High-Temperature Cobalt-Base Alloy
Conicro 5010W has a face-centered cubic structure and is a cobalt-base alloy containing chromium, tungsten, and nickel. The alloy is used in aerospace applications and in the heat-treatment industry. This datasheet provides information on composition, physical properties, and elasticity. It also includes information on forming, heat treating, machining, and joining. Filing Code: CO-103. Producer or source: VDM Technologies Corporation.
Journal Articles
Alloy Digest (1997) 46 (9): Ti-109.
Published: 01 September 1997
... Sandvik Ti-3Al-2.5V Grade 9 titanium-aluminum alloy offers excellent corrosion resistance, especially to chloride media, and has a high strength-to-weight ratio, which is especially suitable for use in aerospace applications. Tubing can be produced having a CSR (contractile strain ratio...
Abstract
View articletitled, SANDVIK Ti-3Al-2.5V GRADE 9: Corrosion-Resistant High-Strength Titanium Alloy
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for article titled, SANDVIK Ti-3Al-2.5V GRADE 9: Corrosion-Resistant High-Strength Titanium Alloy
Sandvik Ti-3Al-2.5V Grade 9 titanium-aluminum alloy offers excellent corrosion resistance, especially to chloride media, and has a high strength-to-weight ratio, which is especially suitable for use in aerospace applications. Tubing can be produced having a CSR (contractile strain ratio) that enhances the fatigue endurance limit. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and bend strength as well as fatigue. It also includes information on corrosion resistance as well as forming, machining, and joining. Filing Code: TI-109. Producer or source: Sandvik.
Journal Articles
Alloy Digest (1997) 46 (10): Fe-115.
Published: 01 October 1997
... Novalloy 280 is a nickel-cobalt steel fastener alloy that was introduced for use in military and aerospace applications, but now is available for general fastener use. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well...
Abstract
View articletitled, NOVALLOY 280: Nickel-Cobalt Steel Fastener Alloy
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for article titled, NOVALLOY 280: Nickel-Cobalt Steel Fastener Alloy
Novalloy 280 is a nickel-cobalt steel fastener alloy that was introduced for use in military and aerospace applications, but now is available for general fastener use. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fatigue. It also includes information on heat treating. Filing Code: FE-115. Producer or source: Nova Machine Products Corporation.
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