200 g/m² (5.9 oz/yd²), aero, non-shift
Due to yarn shortages, there may be delivery bottlenecks for ECC fabrics. Delivery while stocks last.
Fibre: Tenax® HTA 40 E13 / 200 tex (3k), alternatively Pyrofil™ TR30S (carbon fibre according to material performance sheet WLB 8.3611 (high-strength yarns for aerospace applications)
Style 452-5-aero, non-shift
Material as per aviation standards
Width: 100 cm
Setting (Thr./cm): 5 x 5
Basic weight 200 g/m² + 10-15 g/m² EP binder
Supporting parts in aircraft construction, motorsports, marine construction and modelling, carbon design
The fabric is coated on one side with an EP-Binder, backside is smooth.
The EP binder prevents slippage, so cut pieces do not loose threads. Heat (pressure mould) can be used to preform the fabric before impregnation with resin. Specifically for carbon designs in automotive engineering. Even an iron on the surface (eg during coating of surfaces) is possible. The fabric will be formed only and has additionally to be impregnated with resin.
If the fabric is processed during normal hand laminating without melting the binder, please make sure that the smooth side is placed on the later visible side of the mould. Otherwise too many small air bubbles will form because the fabric does not lie flat due to the "droplets" of the EP binder.
Information about application eWiki.
Calculated data for hand laminates with 35 volume per cent fibres:
Resin consumption: 241 g/m², laminate thickness: 0.32 mm, laminate weight: 441 g/m²
all Prices price incl. VAT, possibly plus shipping
Classification of the substance or mixtureThe product is not classified according to the CLP regulation.
Signal word: n/a