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supersonic aircraft application
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Journal Articles
Alloy Digest (1966) 15 (6): SS-183.
Published: 01 June 1966
... Armco PH14-8Mo is a precipitation-hardening stainless steel offering high strength at elevated temperatures along with exceptional toughness and tear resistance. It resists stress corrosion attack. It is recommended for pressure tanks, supersonic aircraft and aerospace applications. This datasheet...
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Armco PH14-8Mo is a precipitation-hardening stainless steel offering high strength at elevated temperatures along with exceptional toughness and tear resistance. It resists stress corrosion attack. It is recommended for pressure tanks, supersonic aircraft 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 high temperature performance and corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: SS-183. Producer or source: Armco Inc., Eastern Steel Division.
Journal Articles
Alloy Digest (1968) 17 (4): SS-208.
Published: 01 April 1968
... Fifth-Vickers F.V. 520(S) is a corrosion resistant martensitic steel which is readily weldable and capable of being hardened by low temperature heat treatment. It is recommended for turbine components and supersonic aircraft parts. This datasheet provides information on composition, physical...
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Fifth-Vickers F.V. 520(S) is a corrosion resistant martensitic steel which is readily weldable and capable of being hardened by low temperature heat treatment. It is recommended for turbine components and supersonic aircraft parts. 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, and joining. Filing Code: SS-208. Producer or source: Firth-Vickers Stainless Steels Ltd.
Journal Articles
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
Alloy Digest (1961) 10 (5): Fe-19.
Published: 01 May 1961
... transformers. General Purpose transformer. Space Factor 95% 4MIL H or Z Type 400 to 2600 cycles: Radio power, filament, rectifier transformers and chokes. Induction beating and ocher electronic trans- former applications. Aircraft power transformers. 90% 2MrL L Type 1 MIL M Tee Above 2600 cycles: Power pulse...
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HIPERSIL is a high permeability silicon-iron alloy recommended for use in transformers. It has low hysteresis loss and preferred orientation. Its superior magnetic qualities exist only in the rolling direction. This datasheet provides information on composition, physical properties, and tensile properties. Filing Code: Fe-19. Producer or source: Westinghouse Electric Corporation.
Journal Articles
Alloy Digest (1965) 14 (8): Al-146.
Published: 01 August 1965
.... Forms Available: Sintered bats, secrions, forgings, sheers, tubes, and sincer-pressed compacts. Applications: Compressor blades, engine components, turbine parts, pistons and piston parts, structural marerial for re- actors, heat exchanger cubes, cylinder heads, skins in supersonic aircraft...
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SAP is a special Sintered Aluminum Powder characterized by high tensile strength at room temperature and at elevated temperatures. It features a range of useful engineering properties. 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, machining, joining, and powder metal forms. Filing Code: Al-146. Producer or source: Aluminium Industrie Atkiengesellschaft.
Journal Articles
Alloy Digest (1960) 9 (12): Ti-28.
Published: 01 December 1960
..., plate, wire. Applications: Missile and supersonic aircraft components, honeycomb structures, rivets, springs, pressure tanks, bolts, fasteners, aircraft skins, airframe members, pressure vessels. Manufacturer: Crucible Steel Company of America, Titanium Division Pittsburgh 30, Pennsylvania ...
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Crucible B-120VCA is a higher performance all-beta titanium alloy. It responds to age-hardening heat treatment and is designed to be stable for at least 1500 hours under stress up to temperatures of 550 F and to substantially higher temperatures for shorter times. This datasheet provides information on composition, physical properties, elasticity, tensile properties, and bend strength as well as creep, and deformation. It also includes information on corrosion resistance as well as forming, heat treating, machining, joining, and surface treatment. Filing Code: Ti-28. Producer or source: Crucible Steel Company of America.
Journal Articles
Alloy Digest (1960) 9 (12): SS-112.
Published: 01 December 1960
... applications where strength and hardness are required such as knife blades, valves, erc. Corrosico resistant springs. Airframe structural members, airframe ducring, nacelles and ocher missile and supersonic aircraft appli- cations. Pressure tanks. power plant components, high pressure ducring. Manufacturer...
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Allegheny Metal 355 is a chromium-nickel-molybdenum stainless steel to bridge the gap between the 300 and 400 series. It can be precipitation hardened by heat treatment. It is best suited for heavy sections. 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 forming, heat treating, machining, joining, and surface treatment. Filing Code: SS-112. Producer or source: Allegheny Ludlum Corporation.