Abstract
Hybrid and ramjet engines became now effective propulsion systems with great development potential in different fields. They require using proper high-energy components. At high-speed blowing conditions conventional polymer fuels exhibit relatively low regression rate. As an alternative, it is proposed to use paraffin and based on it compositions. Paraffin is high-energy hydrocarbon with a low melting point leading to a high regression rate in high-speed blowing conditions. The results of experimental study of regression behavior of paraffin mixtures with various additives under intensive hot air blowing at 1 MPa pressure are presented. Stearic acid, nanoaluminum Alex, aluminum hydride AlH3, B and mechanoactivated aluminum boride AlB2 were used as 10 % by mass additives. Experiments were conducted on cylindrical perforated samples. Using original design microwave gauge the current diameter of a sample bore was measured during experiment with subsequent calculation of regression rate. Based on experimental data and the results of heat balance calculation, the temperature on the gasified surface of paraffin fuel was estimated.
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