Search Results for armor plate

HY-80 is a low carbon, nickel, chromium, molybdenum alloy steel exhibiting moderate strength combined with excellent toughness and ductility at all expected service temperatures. It can be readily welded to form tough weldments. It is supplied in the quenched and tempered condition. It is recommended for pressure hulls of submarines and for ordnance equipment. 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, machining, and joining. Filing Code: SA-197. Producer or source: United States Steel Corporation.

Alcoa Alloy 2519 is an improvement over alloy 2219 in strength. The alloy is an aluminum copper grade and was developed for improved ballistic performance for military vehicles. This datasheet provides information on composition, tensile properties, and compressive strength. It also includes information on joining. Filing Code: AL-370. Producer or source: Alcoa Mill Products Inc.

K12 has a Ni-Mo-Cr alloy steel composition and possesses an appropriate combination of hardness and toughness mandatory for proper ballistics performance. K12 plate is normally supplied in the annealed condition so that it may be more easily cut and formed into the desired configuration. It may also be supplied as heat treated parts cut to the final configuration. This datasheet provides information on physical properties, hardness, tensile properties, and bend strength as well as fracture toughness. It also includes information on corrosion resistance as well as forming and joining. Filing Code: SA-560. Producer or source: Allegheny Ludlum.

ATI 425 was originally developed for hot-rolled armor plate to provide ballistic protection comparable to Ti-6Al-4V and has been evaluated against a variety of projectile threats for use as armor. While processing the alloy for armor plate applications, it was observed that the material exhibited very good hot workability, permitting a more lenient window of processing parameters than necessary for Ti-6Al-4V. Versatility then expanded, and applications now exist in the chemical process industry (CPI) and in the aerospace industry. This datasheet provides information on composition, physical properties, and tensile properties as well as fracture toughness and fatigue. It also includes information on corrosion resistance. Filing Code: TI-133. Producer or source: ATI Wah Chang, Allegheny Technologies. Originally published March 2004, revised July 2004.

JESSOP No. 9, super high tensile steel, is one of the toughest and most wear resistant steels of its class in existence. Primarily developed as a high tensile, non-magnetic armor plate, it has since been widely used for equipment subject to severe battering. This datasheet provides information on composition, physical properties, hardness, and tensile properties as well as fracture toughness and fatigue. It also includes information on forming, heat treating, machining, and joining. Filing Code: SA-457. Producer or source: Jessop Steel Company.

ATI 500-MIL High Hard is a specialty steel of wrought Ni-Cr-Mo specialty steel for armor plate. This datasheet provides information on composition, physical properties, hardness, and tensile properties as well as fracture toughness. It also includes information on forming, heat treating, machining, and joining. Filing Code: SA-606. Producer or source: ATI Defense.

ATI 600-MIL Ultra High Hard is a specialty steel of wrought Ni-Cr-Mo steel for armor plate. This datasheet provides information on composition, physical properties, hardness, and tensile properties. It also includes information on forming, heat treating, machining, and joining. Filing Code: SA-610. Producer or source: ATI Defense.

UNIMACH AF 1410 is a high-strength, high-fracture-resistant iron-based alloy (steel). It exhibits superior toughness over all other high-strength steels and has the highest combination of strength and toughness available in any high-strength alloy. It is recommended for consideration in a wide range of highly-stressed, fracture-critical applications such as airframe structural components, landing gear components and light armor plate. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as fracture toughness. It also includes information on corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: SA-398. Producer or source: Cyclops Corporation.

AA 5456 is a wrought aluminum-magnesium alloy of relatively high strength with good welding characteristics making it suitable for structural applications. (See also Aluminum 5456, Alloy Digest Al-70, September 1958.) This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and shear strength. It also includes information on low temperature performance as well as forming, heat treating, machining, and joining. Filing Code: Al-316. Producer or source: Various aluminum companies.

Armox Advance combines good ballistic properties with excellent toughness. Hardness for Advance is 58-63 HRC. This datasheet provides information on composition and hardness as well as fracture toughness. It also includes information on forming, heat treating, and joining. Filing Code: SA-686. Producer or source: SSAB Armox.

Armox 600T combines good ballistic properties with excellent toughness. Hardness for 600T is 570–640 HBW. This datasheet provides information on composition, hardness, and tensile properties as well as fracture toughness. It also includes information on surface qualities as well as forming, heat treating, and joining. Filing Code: SA-683. Producer or source: SSAB Armox.

LESCALLOY HP 9-4-30 VAC-ARC is a low-alloy, high-strength steel with a high nickel content to promote toughness. It was designated for high hardenability and good weldability. It is produced by the vacuum-consumable-electrode process to insure cleanliness and provide a preferred ingot structure. 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, machining, joining, and surface treatment. Filing Code: SA-343. Producer or source: Latrobe Steel Company.

Alcotec weld filler wire 2319 is a heat treatable wire. The principal alloying elements are copper, manganese, vanadium, zirconium, and titanium. Weld filler wire 2319 was developed primarily for aircraft structural components to weld the high-strength age-hardenable wrought alloy 2219. This datasheet provides information on composition, physical properties, and tensile properties. It also includes information on joining. Filing Code: AL-382. Producer or source: AlcoTec Wire Corporation.

Armox 370T Class 2 combines good ballistic properties with excellent toughness. Hardness for Class 2 is 280-330 HBW for thicknesses up to 150 mm (6 in.). This datasheet provides information on composition, hardness, and tensile properties as well as fracture toughness. It also includes information on forming and joining. Filing Code: SA-677. Producer or source: SSAB Armox.

Alcotec Weld Wire 5356 is a non-heat-treatable wire with moderate high strength capabilities. This datasheet provides information on composition, physical properties, tensile properties, and shear strength. It also includes information on joining. Filing Code: AL-376. Producer or source: AlcoTec Wire Corporation.

Armox 440T combines good ballistic properties with excellent toughness. Hardness is 420-480 HBW. This datasheet provides information on composition, hardness, and tensile properties as well as fracture toughness. It also includes information on forming, machining, and joining. Filing Code: SA-679. Producer or source: SSAB Armox.

MARS 300 is a super high-hardness (620 HB) steel for ballistic protection. This datasheet provides information on composition, physical properties, hardness, and tensile properties as well as fracture toughness. It also includes information on forming, heat treating, machining, and joining. Filing Code: SA-685. Producer or source: Industeel USA, LLC and Industeel France.

Magnesium-LA[4]A is a magnesium-lithium light weight alloy for missile and space vehicle structures. This datasheet provides information on composition, physical properties, hardness, elasticity, tensile properties, and compressive and bearing strength as well as fracture toughness. It also includes information on low and high temperature performance, and corrosion resistance as well as casting, forming, heat treating, machining, and joining. Filing Code: Mg-56. Producer or source: Brooks & Perkins Inc..

Austral Wright 5083 is a wrought, non-heat-treatable, aluminum-magnesium-manganese-chromium alloy (5xxx series). It has the highest strength of the non-heat-treatable alloys but is not recommended for use at temperatures in excess of 65 °C (150 °F). It is among the most widely used aluminum alloys for marine applications. 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, and joining. Filing Code: Al-493. Producer or source: Austral Wright Metals.

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.