Solid fuels for hybrid rockets were characterized in the framework of a research project aimed to develop a new generation of solid fuels, combining at the same time good mechanical and ballistic properties. Original techniques were implemented in order to improve para©n-based fuels. The ¦rst strengthening technique involves the use of a polyurethane foam (PUF); a second technique is based on thermoplastic polymers mixed at molecular level with the para©n binder. A ballistic characterization of para©n-based hybrid rocket solid fuels was performed, considering pure wax-based fuels and fuels doped with suitable metal additives. Nano-Al powders and metal hydrides (magnesium hydride (MgH 2 ), lithium aluminum hydride (LiAlH 4 )) were used as ¦llers in para©n matrices. The results of this investigation show a strong correlation between the measured viscosity of the melted para©n layer and the regression rate: a decrease of viscosity increases the regression rate. This trend is due to the increasing development of entrainment phenomena, which strongly increase the regression rate. Addition of LiAlH 4 (mass fraction 10%) can further increase the regression rate up to 378% with respect to the pure HTPB regression rate, taken as baseline reference fuel. The highest regression rates were found for the Solid Wax (SW) composition, added with 5% MgH 2 mass fraction; at 350 kg/(m 2 s) oxygen mass §ux, the measured regression rate, averaged in space and time, was 2.5 mm/s, which is approximately ¦ve times higher than that of the pure HTPB composition. Compositions added with nanosized aluminum powders were compared with those added with MgH 2 , using gel or solid wax.