The mark Cu-OF, mat. No CW008A, is a copper free of oxygen and deoxidation agents. To the comparable DIN-mark OFCu, mat. No 2.0040 acc. to DIN 1787 : 1973-01 applies: The material is hydrogen resistant and shows very high thermal and electrical conductivity. Tensile strength and Brinell hardness are

NiCr23Fe shows favorable oxidation resistance at high temperatures due to the Al- and high Cr-content. Excellent high-temperature strength and excellent scaling resistance allow application temperatures up to 1200°C (highest application temperatures in air). Favorable resistance to carburization and

Steel 25CrMoS4 is suitable for high loaded parts (also heavy forged parts) of high heat-treatment sections as well as favorable ductility qualities in aircraft, heavy vehicle and machine engineering (e.g. propellershafts, connecting rods, transmission shafts). Lowest application temperature -40°C.

Steel 25CrMoS4 is suitable for parts of high strength and ductility demands and mean and higher heat-treatment sections as well as enhanced workability in vehicle, engine and machine engineering (e.g. crankshafts, steering knuckles, pinions). Lowest application temperature -40°C. As a bright steel

NiCr22Mo9Nb, also contained in VDTÜV-material specification 489 : 1992-03 shows excellent resistance to pitting, crevice, erosion and intercrystalline corrosion. Insensitivity to chloride induced stress corrosion. Favorable resistance to mineral acids, such as nitrous, phosphoric, sulphuric and muri

Steel 25CrMoS4 is suitable for parts of high strength and ductility demands and mean and higher heat-treatment sections as well as enhanced workability in vehicle, engine and machine engineering (e.g. crankshafts, steering knuckles, pinions). Lowest application temperature -40°C. As a bright steel

NiCr20Ti is also contained as a aviation material (mat. No 2.4630) in material-performance specifications of the German Aviation WL 2.4630-1, -2, -3,-4, -100 : 1993-08 (Werkstoff-Leistungsblätter der Deutschen Luftfahrt WL). It is non-scaling up to approx. 1150 °C (highest application temperature in

Cu-DLP, mat. No CW023A, is a deoxidized copper with limited, low residual copper-content. To the comparable DIN-make SW-Cu, mat. No 2.0076 acc. to DIN 1787 : 1973-01 applies: Tensile strength and Brinell hardness are increasable by cold forming. SW-Cu is hydrogen resistant and shows the lowest therm

Cu-DLP, mat. No CW023A, is a deoxidized copper with limited, low residual copper-content. To the comparable DIN-make SW-Cu, mat. No 2.0076 acc. to DIN 1787 : 1973-01 applies: Tensile strength and Brinell hardness are increasable by cold forming. SW-Cu is hydrogen resistant and shows the lowest therm

Hot-dip tinned strip.PropertiesGeneralPropertyTemperatureValueDensity20.0 °C8.9 - 8.94 g/cm³MechanicalPropertyTemperatureValueCommentElastic modulus20.0 °C132 GPaHardness, Brinell20.0 °C105 [-]Hardness, Vickers20.0 °C110 [-]Poisson's ratio20.0 °C0.34 [-]Shear modulus23.0 °C48 GPaTypical for Wro

Steel 20NiCrMoS-2 is suitable for parts in vehicle and machine engineering, that are wear loaded at mean core strength, high ductility and fatigue resistance (e.g. gear wheels, shafts, axles). The show an enhanced workability. Lowest application temperature -60°C, most favorable application area up

= 99,9% and a high residual copper-content. Tensile strength and Brinell hardness are increasable by cold forming. SF-Cu (Cu-DHP) is hydrogen resistant and shows the lowest thermal and electrical conductivity of the pure copper materials. Processing properties: hot forming: very good cold forming:

Steel 20NiCrMoS-2 is suitable for parts in vehicle and machine engineering, that are wear loaded at mean core strength, high ductility and fatigue resistance (e.g. gear wheels, shafts, axles). The show an enhanced workability. Lowest application temperature -60°C, most favorable application area up

CuSn8, mat. No. CW453K, is comparable to the DIN-make CuSn8, mat. No. 2.1030, acc. to DIN 17662 : 1983-12. Properties of the CuSn-alloy are predominantly determined by the tin-content. Tensile strength, yield point and hardness increase according to the rising cold forming grade, elongation after fr

CuSn8, mat. No. CW453K, is comparable to the DIN-make CuSn8, mat. No. 2.1030, acc. to DIN 17662 : 1983-12. Properties of the CuSn-alloy are predominantly determined by the tin-content. Tensile strength, yield point and hardness increase according to the rising cold forming grade, elongation after fr

CuSn6, mat. No. CW425K, is comparable to the DIN-make CuSn6, mat. No. 2.1020, acc. to DIN 17662 : 1983-12. Properties of the CuSn-alloy are predominantly determined by the tin-content. Tensile strength, yield point and hardness increase according to the rising cold forming grade, elongation after fr

CuSn6, mat. No. CW425K, is comparable to the DIN-make CuSn6, mat. No. 2.1020, acc. to DIN 17662 : 1983-12. Properties of the CuSn-alloy are predominantly determined by the tin-content. Tensile strength, yield point and hardness increase according to the rising cold forming grade, elongation after fr

CuSn6, mat. No. CW425K, is comparable to the DIN-make CuSn6, mat. No. 2.1020, acc. to DIN 17662 : 1983-12. Properties of the CuSn-alloy are predominantly determined by the tin-content. Tensile strength, yield point and hardness increase according to the rising cold forming grade, elongation after fr

CuSn6, mat. No. CW425K, is comparable to the DIN-make CuSn6, mat. No. 2.1020, acc. to DIN 17662 : 1983-12. Properties of the CuSn-alloy are predominantly determined by the tin-content. Tensile strength, yield point and hardness increase according to the rising cold forming grade, elongation after fr

Material CuSn5, mat. No. CW451K is used in the form of tubes for manometer springs or hose tubes as well as for contact springs and connectors. Basically the same application area as CuSn6 (CW452K). CuSn5 shows slightly higher electrical conductivity at slightly lower strength due to the lower tin-c