Lowering the burning rate temperature coefficient of composite propellant by compensating its burning surface through thermal expansion and contraction in microstructure
Suhang Chen, Zhenhua Tang, Kui Tang, Lianpeng Cui, Zhao Qin, Kangzhen Xu
Topics & Concepts
Ammonium perchloratePropellantThermal expansionMaterials scienceMicrostructureThermal decompositionComposite materialTemperature coefficientComposite numberAnalytical Chemistry (journal)Chemical engineeringChemistryChromatographyOrganic chemistryEngineeringEnergetic Materials and CombustionRocket and propulsion systems researchThermal and Kinetic Analysis