RESUMO
Carboxylated GAP copolymers (polyGA-carboxylate) compounds (1-7), were synthesized by the simultaneous substitution reaction with PECH, sodium azide, and sodium carboxylate in DMSO. The synthesized compounds (1-7) were characterized by various analysis tools, such as Fourier transform infrared (FT-IR), inverse gated decoupling 13C-nuclear magnetic resonance (13C NMR), gel permeation chromatography (GPC), thermogravimetric analysis (TGA), differential scanning calorimetry (DSC), calorimetry, and friction and impact sensitivity. These poly(GA-carboxylate) compounds (1-7) have better thermal properties owing to their lower glass transition temperatures, from -48 °C to -55 °C, compared to glycidyl azide polymer (GAP) (-49 °C) and similar first thermal decomposition temperatures (228-230 °C) in comparison to GAP (227 °C), regardless of the introduction of the carboxylate group in GAP. Moreover, poly(GA0.8-butyrate0.2) and poly(GA0.8-decanoate0.2) have higher heats of combustion (2331 and 2976 kJ mol-1) and negative formation enthalpies (-0.75 and -2.02 kJ g-1), while GAP has a lower heat of combustion (2029 kJ mol-1) and positive formation enthalpy (1.33 kJ g-1). Therefore, poly(GA-carboxylate) could be a good candidate for the polymeric binder in solid propellants.