Decomposition and combustion of HTPB-based composite propellants containing intercalated HMX crystals with desired high energy but low burn rate
Zikangping Wang, Xue Zhi-hua, Ke‐Juan Meng, Xuexue Zhang, Qi‐Long Yan
Topics & Concepts
CombustionPropellantExothermic reactionMaterials scienceThermal decompositionComposite numberBurn rate (chemistry)DecompositionEnergetic materialAdiabatic flame temperatureExplosive materialChemical engineeringChemistryComposite materialPhysical chemistryOrganic chemistryCombustorEngineeringEnergetic Materials and CombustionThermal and Kinetic AnalysisRocket and propulsion systems research