2012Journal of Propulsion TechnologyOpen access

Investigation on the Combustion Behavior of CMDB Propellant with Mg/Al Alloy

Xiaohong Zhang

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Abstract

The particle size and distribution of particle size of Mg/Al were analyzed by Mastersizer.The thermal characterisitics of CDMB propellant were analyzed by TG-DSC.The flame structure was studied by using the burning device and the differences of the flame structure were compared amongst CMDB,Al-CMDB,Mg-CMDB and Mg/Al-CMDB propellants.The surface appearance of the propellant quenched and surface composition were researched by the SEM and EDS.The results show that the Mg/Al alloy has a peak 630.3℃ of the heat of CMDB propellant.The combustion condition of CMDB propellant with Mg/Al is changed.Meanwhile,the metallic Al fuel combustion efficiency is improved.

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What this paper is about

The particle size and distribution of particle size of Mg/Al were analyzed by Mastersizer.The thermal characterisitics of CDMB propellant were analyzed by TG-DSC.The flame structure was studied by using the burning device and the differences of the flame structure were compared amongst CMDB,Al-CMDB,Mg-CMDB and Mg/Al-CMDB propellants.The surface appearance of the propellant quenched and surface composition were researched by the SEM and EDS.The results show that the Mg/Al alloy has a peak 630.3℃ of the heat of CMDB propellant.The combustion condition of CMDB propellant with Mg/Al is changed.Meanwhile,the metallic Al fuel combustion efficiency is improved.

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Available abstract

The particle size and distribution of particle size of Mg/Al were analyzed by Mastersizer.The thermal characterisitics of CDMB propellant were analyzed by TG-DSC.The flame structure was studied by using the burning device and the differences of the flame structure were compared amongst CMDB,Al-CMDB,Mg-CMDB and Mg/Al-CMDB propellants.The surface appearance of the propellant quenched and surface composition were researched by the SEM and EDS.The results show that the Mg/Al alloy has a peak 630.3℃ of the heat of CMDB propellant.The combustion condition of CMDB propellant with Mg/Al is changed.Meanwhile,the metallic Al fuel combustion efficiency is improved.

Key concepts: Propellant, Materials science, Combustion, Alloy, Particle (ecology), Composite material, Particle size, Metallurgy

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