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missiles components

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Journal Articles
Alloy Digest (1985) 34 (6): Al-258.
Published: 01 June 1985
... ALUMINUM A356.0 is a sand and permanent-mold casting alloy. It responds to an age-hardening heat treatment. This alloy has a relatively good combination of strength and ductility in the solution-treated and aged condition. Aluminum A356.0 is recommended for aircraft and missile components where...
Journal Articles
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...
Journal Articles
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...
Journal Articles
Alloy Digest (1966) 15 (4): Ti-47.
Published: 01 April 1966
... 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...
Journal Articles
Alloy Digest (1967) 16 (6): Mg-63.
Published: 01 June 1967
... 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...
Journal Articles
Alloy Digest (1968) 17 (1): Cb-14.
Published: 01 January 1968
... Columbium SCB-291 is a columbium-base alloy having excellent high temperature properties and good fabricability. It is recommended for nuclear reactors, space vehicles, jet and missile components. This datasheet provides information on composition, physical properties, hardness, and tensile...
Journal Articles
Alloy Digest (1981) 30 (6): Cb-7.
Published: 01 June 1981
... FANSTEEL 85 METAL is a columbium-base alloy characterized by good fabricability at room temperature, good weldability and a good combination of creep strength and oxidation resistance at elevated temperatures. Its applications include missile and rocket components and many other high-temperature...
Journal Articles
Alloy Digest (1978) 27 (11): Ni-258.
Published: 01 November 1978
... 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...
Journal Articles
Alloy Digest (1976) 25 (5): Al-223.
Published: 01 May 1976
... 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...
Journal Articles
Alloy Digest (1979) 28 (4): Al-234.
Published: 01 April 1979
... 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...
Journal Articles
Alloy Digest (1982) 31 (5): Al-238.
Published: 01 May 1982
... 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...
Journal Articles
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...
Journal Articles
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...
Journal Articles
Alloy Digest (1966) 15 (3): Ni-112.
Published: 01 March 1966
... 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...
Journal Articles
Alloy Digest (1966) 15 (10): Cb-11.
Published: 01 October 1966
... 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...
Journal Articles
Alloy Digest (1963) 12 (5): SA-146.
Published: 01 May 1963
... 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...
Journal Articles
Alloy Digest (1986) 35 (11): SS-478.
Published: 01 November 1986
... 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 I 200 F. It is used for various high-temperature applications such as components for jet engines. gas turbines. turbochargers and missiles...
Journal Articles
Alloy Digest (1966) 15 (5): Mg-59.
Published: 01 May 1966
... 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...
Journal Articles
Alloy Digest (1969) 18 (7): Al-188.
Published: 01 July 1969
...-hardening heat treatment for increased strength and hardness. Forms Available: Ingots. sand and permanent mold castings. Applications: Aircraft and missile components. structural parts. Manufacturer: Kaiser Aluminum & Chemical Corp.. Oakland. California Aluminum Co. of America, Pittsburgh. Pennsylvania...
Journal Articles
Alloy Digest (1960) 9 (4): Mg-46.
Published: 01 April 1960
... user as is the case of HK3lA-T6. In addition it has superior creep strength over HK31A-T6. HMZlA-T5 forgings are also available. Forms Available: Sheets, plates and forgings. Applications: Aircraft and missile components. Manufacturer: The Dow Metal Products Company, Division of The Dow Chemical...