PropertiesGeneralPropertyValueConditionRelated StandardsDensity2.7 g/cm³FEN 573-3, EN 1715-3, EN 570MechanicalPropertyValueConditionRelated StandardsCommentElastic modulus70.0 GPaFEN 573-3, EN 1715-3, EN 570Hardness, Brinell18.0 [-]FEN 573-3, EN 570Plane-Strain Fracture Toughnes22.0 - 35.0 MPa·√mTyp

PropertiesGeneralPropertyValueConditionRelated StandardsDensity2.7 g/cm³T6AA Standards, ASTM B221MechanicalPropertyValueConditionRelated StandardsCommentElastic modulus70.0 GPaTypical for Wrought 6000 Series AluminiumPlane-Strain Fracture Toughnes22.0 - 35.0 MPa·√mTypical for Wrought 6000 Series Alu

PropertiesGeneralPropertyValueConditionRelated StandardsDensity2.7 g/cm³T5AA Standards, ASTM B221MechanicalPropertyValueConditionRelated StandardsCommentElastic modulus70.0 GPaTypical for Wrought 6000 Series AluminiumPlane-Strain Fracture Toughnes22.0 - 35.0 MPa·√mTypical for Wrought 6000 Series Alu

PropertiesGeneralPropertyValueConditionRelated StandardsDensity2.71 g/cm³T4AA StandardsMechanicalPropertyValueConditionRelated StandardsCommentElastic modulus70.0 GPaTypical for Wrought 6000 Series AluminiumPlane-Strain Fracture Toughnes22.0 - 35.0 MPa·√mTypical for Wrought 6000 Series AluminiumPois

Alloy 165 provides strength close to that of Alloy 25, with slightly lower beryllium content. The alloy features high fatigue strength and resistance to wear, corrosion, galling, and stress relaxation.PropertiesGeneralPropertyTemperatureValueDensity23.0 °C8.41 g/cm³MechanicalPropertyTemperatureValue

Alloy 165 provides strength close to that of Alloy 25, with slightly lower beryllium content. The alloy features high fatigue strength and resistance to wear, corrosion, galling, and stress relaxation.PropertiesGeneralPropertyTemperatureValueDensity23.0 °C8.41 g/cm³MechanicalPropertyTemperatureValue

Alloy 25 from Materion Performance Alloys provides the highest strength of any copper alloy, with electrical and thermal conductivity considerably greater than other high strength copper alloys. The alloy features high fatigue strength and resistance to wear, corrosion, galling, and stress relaxatio

Alloy 25 from Materion Performance Alloys provides the highest strength of any copper alloy, with electrical and thermal conductivity considerably greater than other high strength copper alloys. The alloy features high fatigue strength and resistance to wear, corrosion, galling, and stress relaxatio

Properties: - in hardened state resistant to water and steam - in annealed or high tempered state corrosion resitance is not sufficient - application in hardened state with fine grounded or polished surface Application: - for manufacturing cutting tools (knife blades, scissors, surgical instruments)

Material X7CrNiAl17-7 is comparable to X 7 CrNiAl 17 7 acc. to DIN17224 : 1982-02. The material is a hardenable stainless steel with high strength and hardness, sufficient corrosion resistance and satisfactory workability. It shows the lowest corrosion resistance within the group of type 1.4301 owin

The martensitic (special grade) X29S13 is well machinable and used for turned parts.PropertiesGeneralPropertyTemperatureValueDensity20.0 °C7.7 g/cm³MechanicalPropertyTemperatureValueCommentElastic modulus20.0 °C215 GPa100.0 °C212 GPa200.0 °C205 GPa300.0 °C200 GPa400.0 °C190 GPaElongation20.0 °C8 - 1

6 mm. Large-scale application for welded parts in chemical apparatus engineering as well as in food, luxury food, fat and soap industry, in film and photo industrie, in leather and sugar factories and for household articles. Application up to 550 °C, if there are no media causing intercrystalline at

The steel is used for rail vehicle engineering acc. to the selected standard DIN 5512-1.The corresponding properties of EN 10025-2 shall be taken.PropertiesGeneralPropertyTemperatureValueCommentDensity23.0 °C7.8 - 7.9 g/cm³Typical for Medium Carbon SteelMechanicalPropertyTemperatureValueCommentElast

According to VdTÜV-Werkstoffblatt 345 : 1999-06, the material LC-Ni99 with the material number 2.4068 is applied for pressure vessels according to TRB 100 and AD-Merkblatt from -10 to 600 °C. Besides, the pure-nickel material is used for ranges of applications in nuclear engineering as far as the ru

The austenitic steel X6CrNiCuS18-9-2 is used in solution annealed condition in the form of rods, wire rod and profiles. It is not resistant to intercrystalline corrosion.PropertiesGeneralPropertyTemperatureValueDensity20.0 °C7.9 g/cm³MechanicalPropertyTemperatureValueCommentElastic modulus20.0 °C200

PropertiesGeneralPropertyTemperatureValueDensity20.0 °C7.93 g/cm³MechanicalPropertyTemperatureValueCommentElastic modulus-100.0 °C206 GPa20.0 °C196 GPa100.0 °C190 GPa200.0 °C182 GPa300.0 °C174 GPa400.0 °C166 GPa500.0 °C158 GPa600.0 °C150 GPa700.0 °C142 GPa800.0 °C134 GPa900.0 °C127 GPa1000.0 °C120 G

The material LC-NiCr15Fe with the material number 2.4817 is applied in the form of strips, sheets, tubes, bars, wires and forgings for corrosion-resistant construction components. It is similar to the material NiCr15Fe (material number 2.4816), yet with a very low carbon content, and it shows excell

Trademark X2CrNiMo18-14-3 is comparable to X 2 CrNiMo 18 14 3 acc. to DIN 17440-85. This material is a variant of 1.4404 with slightly increased alloying contents for Cr, Ni and Mo, thus improved corrosion properties. It is resistant to intercrystalline corrosion, also in sensitized condition. Appli

PropertiesGeneralPropertyTemperatureValueDensity20.0 °C7.85 g/cm³MechanicalPropertyTemperatureValueCommentElastic modulus-100.0 °C217 GPa20.0 °C212 GPa100.0 °C207 GPa200.0 °C199 GPa300.0 °C192 GPa400.0 °C184 GPa500.0 °C175 GPa600.0 °C164 GPaElongation20.0 °C28 %Poisson's ratio20.0 °C0.28 [-]She

High-temperature resistant nickel alloy, sheet and strip, forgings and bars- hardenable- high-temperature resistant- resistant to scaling- well cold formable- well weldable- badly splinterableApplication:- Combustion chambers- Turbine casesPropertiesGeneralPropertyTemperatureValueDensity20.0 °C8.36