PropertiesGeneralPropertyValueConditionRelated StandardsDensity2.71 g/cm³H38EN 573-3, EN 1592, EN 485MechanicalPropertyValueConditionRelated StandardsCommentElastic modulus70.0 GPaH38EN 573-3, EN 1592, EN 485Hardness, Brinell87.0 [-]H38EN 573-3, EN 485Plane-Strain Fracture Toughnes22.0 - 35.0 MPa·√m

0,6%) causes an increase of the heat resistance (up to 150°C) of the material and the recrystallisation limit. The result of the last is, that in case of extruded profiles the strength in longitudinal direction increases. The material is characterised by a good corrosion resistance. It is sea water

PropertiesGeneralPropertyValueConditionRelated StandardsDensity2.71 g/cm³H17EN 573-3, EN 754MechanicalPropertyValueConditionRelated StandardsCommentElastic modulus70.0 GPaH17EN 573-3, EN 754Hardness, Brinell85.0 [-]H17EN 573-3, EN 754Plane-Strain Fracture Toughnes22.0 - 35.0 MPa·√mTypical for Wrough

PropertiesGeneralPropertyValueConditionRelated StandardsDensity2.71 g/cm³H15EN 573-3, EN 754MechanicalPropertyValueConditionRelated StandardsCommentElastic modulus70.0 GPaH15EN 573-3, EN 754Hardness, Brinell80.0 [-]H15EN 573-3, EN 754Plane-Strain Fracture Toughnes22.0 - 35.0 MPa·√mTypical for Wrough

PropertiesGeneralPropertyValueConditionRelated StandardsDensity2.71 g/cm³H13EN 573-3, EN 754MechanicalPropertyValueConditionRelated StandardsCommentElastic modulus70.0 GPaH13EN 573-3, EN 754Hardness, Brinell70.0 [-]H13EN 573-3, EN 754Plane-Strain Fracture Toughnes22.0 - 35.0 MPa·√mTypical for Wrough

PropertiesGeneralPropertyValueConditionRelated StandardsDensity2.71 g/cm³H112EN 573-3, EN 485, EN 755MechanicalPropertyValueConditionRelated StandardsCommentElastic modulus70.0 GPaH112EN 573-3, EN 485, EN 755Hardness, Brinell50.0 [-]H112EN 573-3, EN 75552.0 [-]H112EN 573-3, EN 48558.0 [-]H112EN 573-

The alloy Al99,85Mg1 belongs to the standardised glossing materials. It can be polished after preceding mechanical polishing chemically or electrolytically to high gloss. For using the high gloss surface a afterwards anodising is necessary. The degree of arranged reflection (gloss degree) dependents

The alloy Al99,85Mg1 belongs to the standardised glossing materials. It can be polished after preceding mechanical polishing chemically or electrolytically to high gloss. For using the high gloss surface a afterwards anodising is necessary. The degree of arranged reflection (gloss degree) dependents

The alloy Al99,9Mg0,5 belongs to the standardised glossing materials. It can be polished after preceding mechanical polishing chemically or electrolytically to high gloss. For using the high gloss surface a afterwards anodising is necessary. The degree of arranged reflection (gloss degree) dependent

The alloy Al99,9Mg0,5 belongs to the standardised glossing materials. It can be polished after preceding mechanical polishing chemically or electrolytically to high gloss. For using the high gloss surface a afterwards anodising is necessary. The degree of arranged reflection (gloss degree) dependent

The alloy Al99,9Mg0,5 belongs to the standardised glossing materials. It can be polished after preceding mechanical polishing chemically or electrolytically to high gloss. For using the high gloss surface a afterwards anodising is necessary. The degree of arranged reflection (gloss degree) dependent

The alloy Al99,85Mg0,5 belongs to the standardised glossing materials. It can be polished after preceding mechanical polishing chemically or electrolytically to high gloss. For using the high gloss surface a afterwards anodising is necessary. The degree of arranged reflection (gloss degree) dependen

The alloy Al99,85Mg0,5 belongs to the standardised glossing materials. It can be polished after preceding mechanical polishing chemically or electrolytically to high gloss. For using the high gloss surface a afterwards anodising is necessary. The degree of arranged reflection (gloss degree) dependen

DIN 3.3211 is a readily available alloy that has good surface finish and ability to be anodized.Easy of weldability and brazability with nice surface finish. Resistance to corrosion from seawater and atmospheric conditions. Suitable for hot forging.PropertiesGeneralPropertyTemperatureValueConditionR

DIN 3.3211 is a readily available alloy that has good surface finish and ability to be anodized.Easy of weldability and brazability with nice surface finish. Resistance to corrosion from seawater and atmospheric conditions. Suitable for hot forging.PropertiesGeneralPropertyValueConditionRelated Stan

The alloy Al99,9MgSi belongs to the standardised aluminum shining materials. Aluminum alloys being based on aluminum with a minimum purity of 99,85 %, can be polished after mechanical polishing chemically or electrolytically to high gloss. The produced gloss degree must, in order to remain preserved

DIN 3.4365 is a high-strength alloy that offers good stress-corrosion cracking resistance. Known as a mainstay in the aerospace industry since it was introduced, Aluminum 7075 brings moderate toughness as well as an excellent strength-to-weight ratio. It is also important to note that at sub-zero te

The alloy AlZnMgCu0,5 belongs to the aluminum materials, which achieve very high mechanical strength. With hot ageing the strength grade F 49 is attainable. This alloy is good splinter-giving machinably. The alloy is weldable with consideration of certain conditions, especially a heat influence zone

The alloy AlZnMgCu0,5 belongs to the aluminum materials, which achieve very high mechanical strength. With hot ageing the strength grade F 49 is attainable. This alloy is good splinter-giving machinably. The alloy is weldable with consideration of certain conditions, especially a heat influence zone

The alloy AlZnMgCu0,5 belongs to the aluminum materials, which achieve very high mechanical strength. With hot ageing the strength grade F 49 is attainable. This alloy is good splinter-giving machinably. The alloy is weldable with consideration of certain conditions, especially a heat influence zone