1-20 of 94 Search Results for

aircraft-missile applications

Follow your search
Access your saved searches in your account

Would you like to receive an alert when new items match your search?
Close Modal
Sort by
Journal Articles
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...
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 (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...
Journal Articles
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, and...
Journal Articles
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...
Journal Articles
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...
Journal Articles
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...
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 (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...
Journal Articles
Alloy Digest (1966) 15 (5): Mg-59.
Published: 01 May 1966
... at elevated temperatures. 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...
Journal Articles
Alloy Digest (1965) 14 (5): SS-168.
Published: 01 May 1965
... bulletin 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...
Journal Articles
Alloy Digest (1982) 31 (5): Al-238.
Published: 01 May 1982
... this resis- tance can be improved 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...
Journal Articles
Alloy Digest (1967) 16 (6): Mg-63.
Published: 01 June 1967
... pressures up to 3000 psi. 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 ...
Journal Articles
Alloy Digest (1966) 15 (4): Ti-47.
Published: 01 April 1966
... 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 ...
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 (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 (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 (1963) 12 (5): SA-146.
Published: 01 May 1963
... and missile systems. Srrength 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...
Journal Articles
Alloy Digest (1978) 27 (10): TS-339.
Published: 01 October 1978
... wear resistance. This steel has also found wide application as an aircraft structural material for critical components in aircraft and missiles. It can be used at ves high strength levels in excess of 260,000 psi (18,300 kg/ cm ). It also shows high creep and rupture strength at temper- atures between...
Journal Articles
Alloy Digest (1981) 30 (7): Ni-269.
Published: 01 July 1981
... successfully, using low speeds and heavy feeds to avoid excessive work hardening. Hot forging presents no unusual problems and the alloy can be welded. Forms Available: Billets, bars, rods, sheet, strip, wire, tubing and forgings. Applications: Aircraft gas turbine and compressor components, bolts, screws...