UNIMAR 250 is a maraging alloy steel having high strength, good notch toughness, excellent cryogenic properties and deep hardenability. It is recommended for pressure vessels, solid-fuel rocket cases and pressure bottles, landing-gear components, processing equipment operating in the temperature range of 300 to 600 F, and components for spacecraft, jet engines and gas turbines. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties as well as fracture toughness and fatigue. It also includes information on high temperature performance and corrosion resistance as well as forming, heat treating, machining, and joining. Filing Code: SA-304. Producer or source: Cyclops Corporation.

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, physical properties, elasticity, and tensile properties as well as fracture toughness and 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: Cb-11. Producer or source: Wah Chang.

Magnesium-LA91 is a magnesium-lithium lightweight alloy recommended for missile and space vehicle structures. This datasheet provides information on composition, physical properties, hardness, elasticity, and tensile properties. It also includes information on corrosion resistance as well as forming, machining, and joining. Filing Code: Mg-58. Producer or source: Brooks & Perkins Inc..

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..

Alcoa 2099-T86 is a low density, high strength plate alloy available in the T86 temper. This datasheet provides information on composition, physical properties, tensile properties, and compressive strength as well as fracture toughness and fatigue. It also includes information on corrosion resistance as well as forming. Filing Code: Al-450. Producer or source: Alcoa Aerospace and Automotive Products.

6092/SiC/17.5P is a discontinuous metal-matrix composite fully characterized for discontinuously reinforced alloy (DRA) structural applications. The base alloy is Aluminum Association 6092, and the reinforcement material is SiC. This datasheet provides information on composition, physical properties, tensile properties, and compressive, shear, and bearing strength as well as fatigue. It also includes information on as well as machining and surface treatment. Filing Code: AL-359. Producer or source: DWA Aluminum Composites.

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.

Haynes Ti-3Al-2.5V alloy is used where the strength/weight ratio is of prime importance; the alloy is 43% lighter than 21-6-9 stainless steel. It is most often used in the form of seamless tubing for aircraft hydraulic systems. This datasheet provides information on composition, physical properties, and tensile properties. It also includes information on forming, heat treating, and joining. Filing Code: TI-145. Producer or source: Haynes International Inc.

CABOT Ti-3A1-2.5V alloy is both lightweight and strong. It has a high strength-to-weight ratio which provides a major design advantage saving weight. It can be formed readily and it has good weldability. Seamless tubing of CABOT Ti-3A1-2.5V was developed for aircraft hydraulic and fuel systems and its performance has been proved by use in various types of aircraft and aerospace vehicles. CABOT Ti-3A1-2.5V is available as plate, sheet and seamless tubing and pipe. This datasheet provides information on composition, physical properties, elasticity, and tensile properties. It also includes information on forming, heat treating, machining, and joining. Filing Code: Ti-85. Producer or source: Cabot Wrought Products.

COLUMBIUM C-129Y is a columbium-tungsten-hafnium refractory alloy having good high temperature properties along with good heat and oxidation resistance. It is recommended for missiles, space craft and various high temperature applicatios. This datasheet provides information on composition, physical properties, elasticity, and tensile properties as well as creep and fatigue. It also includes information on forming, heat treating, machining, and joining. Filing Code: Cb-16. Producer or source: Wah Chang, a Teledyne Corporation.

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.