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The heat decompose mechanism of HTPB propellant was discussed in micro-structure. A meso-hotspot physical model was established combining chemical kinetics, heat transfer, and AP interface evolving. The proceeding of Heat Decompose of HTPB propellant was simulated. The results show that simulation results were consistent with experimental results. The nature of heat decompose processing of HTPB propellant was discovered.

Study on Pyrolytic Mechanism of Composite Solid Propellant Based on Meso Hot Spot Model