Our carbon hybrid panels are manufactured using the thermal high-pressure hot-press process and therefore have a high fiber volume content of >65%. An epoxy resin matrix serves as the matrix material. The carbon hybrid plates are made entirely of carbon fabric with top layers of an aluminized hybrid fabric. The fiber structure has a homogeneous, biaxial fiber distribution in 0°/90°.The hybrid fabric of the outer layers is made in a twill weave, has a smooth, milled surface and has the typical visible fabric structure.Due to the high pressing pressure during the manufacturing process, these carbon hybrid plates achieve outstanding properties in the area of ​​flexural strength as well as torsional and dimensional stability.The panels have the following characteristic laminate values:Flexural strength EN2562: 820 MPaFlexural modulus EN2562: 55 GPaTensile strength ISO 527: 630 MPaTensile modulus of elasticity ISO 527: 58 GPaCoefficient of thermal expansion: 1 E^-06 1/KI.L.S.S. EN2563: ~68MPaDensity: 1.6 g/cm³Fiber weight percentage: >65%Glass transition temperature (short term): 130°C (180°C)Water absorption: < 0.04%

Our carbon hybrid panels are manufactured using the thermal high-pressure hot-press process and therefore have a high fiber volume content of >65%. An epoxy resin matrix serves as the matrix material. The carbon hybrid plates are made entirely of carbon fabric with top layers of an aluminized hybrid fabric. The fiber structure has a homogeneous, biaxial fiber distribution in 0°/90°.The hybrid fabric of the outer layers is made in a twill weave, has a smooth, milled surface and has the typical visible fabric structure.Due to the high pressing pressure during the manufacturing process, these carbon hybrid plates achieve outstanding properties in the area of ​​flexural strength as well as torsional and dimensional stability.The panels have the following characteristic laminate values:Flexural strength EN2562: 820 MPaFlexural modulus EN2562: 55 GPaTensile strength ISO 527: 630 MPaTensile modulus of elasticity ISO 527: 58 GPaCoefficient of thermal expansion: 1 E^-06 1/KI.L.S.S. EN2563: ~68MPaDensity: 1.6 g/cm³Fiber weight percentage: >65%Glass transition temperature (short term): 130°C (180°C)Water absorption: < 0.04%

Our carbon hybrid panels are manufactured using the thermal high-pressure hot-press process and therefore have a high fiber volume content of >65%. An epoxy resin matrix serves as the matrix material. The carbon hybrid plates are made entirely of carbon fabric with top layers of an aluminized hybrid fabric. The fiber structure has a homogeneous, biaxial fiber distribution in 0°/90°.The hybrid fabric of the outer layers is made in a twill weave, has a smooth, milled surface and has the typical visible fabric structure.Due to the high pressing pressure during the manufacturing process, these carbon hybrid plates achieve outstanding properties in the area of ​​flexural strength as well as torsional and dimensional stability.The panels have the following characteristic laminate values:Flexural strength EN2562: 820 MPaFlexural modulus EN2562: 55 GPaTensile strength ISO 527: 630 MPaTensile modulus of elasticity ISO 527: 58 GPaCoefficient of thermal expansion: 1 E^-06 1/KI.L.S.S. EN2563: ~68MPaDensity: 1.6 g/cm³Fiber weight percentage: >65%Glass transition temperature (short term): 130°C (180°C)Water absorption: < 0.04%

Our carbon hybrid panels are manufactured using the thermal high-pressure hot-press process and therefore have a high fiber volume content of >65%. An epoxy resin matrix serves as the matrix material. The carbon hybrid plates are made entirely of carbon fabric with top layers of an aluminized hybrid fabric. The fiber structure has a homogeneous, biaxial fiber distribution in 0°/90°.The hybrid fabric of the outer layers is made in a twill weave, has a smooth, milled surface and has the typical visible fabric structure.Due to the high pressing pressure during the manufacturing process, these carbon hybrid plates achieve outstanding properties in the area of ​​flexural strength as well as torsional and dimensional stability.The panels have the following characteristic laminate values:Flexural strength EN2562: 820 MPaFlexural modulus EN2562: 55 GPaTensile strength ISO 527: 630 MPaTensile modulus of elasticity ISO 527: 58 GPaCoefficient of thermal expansion: 1 E^-06 1/KI.L.S.S. EN2563: ~68MPaDensity: 1.6 g/cm³Fiber weight percentage: >65%Glass transition temperature (short term): 130°C (180°C)Water absorption: < 0.04%

Our carbon hybrid panels are manufactured using the thermal high-pressure hot-press process and therefore have a high fiber volume content of >65%. An epoxy resin matrix serves as the matrix material. The carbon hybrid plates are made entirely of carbon fabric with top layers of an aluminized hybrid fabric. The fiber structure has a homogeneous, biaxial fiber distribution in 0°/90°.The hybrid fabric of the outer layers is made in a twill weave, has a smooth, milled surface and has the typical visible fabric structure.Due to the high pressing pressure during the manufacturing process, these carbon hybrid plates achieve outstanding properties in the area of ​​flexural strength as well as torsional and dimensional stability.The panels have the following characteristic laminate values:Flexural strength EN2562: 820 MPaFlexural modulus EN2562: 55 GPaTensile strength ISO 527: 630 MPaTensile modulus of elasticity ISO 527: 58 GPaCoefficient of thermal expansion: 1 E^-06 1/KI.L.S.S. EN2563: ~68MPaDensity: 1.6 g/cm³Fiber weight percentage: >65%Glass transition temperature (short term): 130°C (180°C)Water absorption: < 0.04%

Our carbon hybrid panels are manufactured using the thermal high-pressure hot-press process and therefore have a high fiber volume content of >65%. An epoxy resin matrix serves as the matrix material. The carbon hybrid plates are made entirely of carbon fabric with top layers of an aluminized hybrid fabric. The fiber structure has a homogeneous, biaxial fiber distribution in 0°/90°.The hybrid fabric of the outer layers is made in a twill weave, has a smooth, milled surface and has the typical visible fabric structure.Due to the high pressing pressure during the manufacturing process, these carbon hybrid plates achieve outstanding properties in the area of ​​flexural strength as well as torsional and dimensional stability.The panels have the following characteristic laminate values:Flexural strength EN2562: 820 MPaFlexural modulus EN2562: 55 GPaTensile strength ISO 527: 630 MPaTensile modulus of elasticity ISO 527: 58 GPaCoefficient of thermal expansion: 1 E^-06 1/KI.L.S.S. EN2563: ~68MPaDensity: 1.6 g/cm³Fiber weight percentage: >65%Glass transition temperature (short term): 130°C (180°C)Water absorption: < 0.04%