Burning characteristics and combustion wave model of AP/AN-based laser-controlled solid propellant

Laser-controlled solid propellant (LCSP) is a novel composite propellant that can achieve non -selfsustaining combustion under laser irradiation. Accordingly, a laser-controlled solid propellant based on AP/AN was designed. The thermal decomposition of LCSP was identified by TG/DSC coupled with MS/ FTIR. It was found that the pyrolyzed gas products of LCSP were mainly composed of N-2, N2O, NH3, CO2, H2O and HCl, etc. Furthermore, the combustion performance parameters including burning rate, ignition delay time, chamber pressure and conducting current of combustion products were tested. As the laser power density increased from 0.42 W/mm(2) to 1.06 W/mm2, the burning rate increased from 0.51 mm/s to 0.88 mm/s and the platform pressure increased from 0.47 KPa to 0.78 KPa, while the ignition delay time decreased from 0.76 s to 0.23 s. Combining with the thermocouple, the combustion wave structure of LCSP can be divided into: pre-heating zone, condensed phase, optical-thermal reaction zone, dark zone and flame zone. Meanwhile, the high laser power density reduced the thickness of condensed phase and increased the thickness of dark zone. Finally, we inferred the combustion model of LCSP and proposed the hypothesis of critical combustion energy to explain the mechanism of non-self-sustaining combustion. (C) 2022 Elsevier Ltd. All rights reserved.

Automated summary

The combustion performance and pyrolyzed gas products of a laser-controlled solid propellant based on AP/AN were studied. Experimental results showed that the burning rate and chamber pressure increased, while the ignition delay time decreased as the laser power density increased. The combustion wave structure was analyzed, and a combustion model and hypothesis of critical combustion energy for non-self-sustaining combustion were proposed.