Abstract

The present work investigates the ablative, thermal and dynamic mechanical properties of epoxy resin modified with nano-titanium dioxide and organomodified monmorillonite. The composites properties with aramid honeycomb core as stiffness reinforcement were compared with those without honeycomb. Samples have been subjected to combustions gases at a temperature above 1900 °C during 120 s. The best thermal protective properties, i.e. the lowest: temperature of the rear surface area and ablative weight loss were exhibited by the composites containing 3.75% of oMMT and 1.25% of TiO2 with aramid honeycomb core. Dynamic mechanical thermal analyser measurements were carried out on an Instrument DMA SDTA861. The tests were performed by using a compression deformation mode in the temperature range from 20 °C to 140 °C. The glass transition temperature (Tg) was determined from the position of the maximum value of tan δ. This temperature reached values from about 74 °C (with tan δ = 0.59) to 79 °C (for tan δ = 0.66). The highest values of the complex modulus M* were in the range from 70 MPa to 465 MPa, for all phase compositions, but at temperature of 140 °C the complex modulus M* had much lower values in the range of 20–25 MPa.

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