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- W2750664401 abstract "In order to investigate the effects of hexachlorocyclotriphosphazene(HCCT)as reducing rate agent on the burning rate,chemical stability,heat of detonation,mechanical sensitivity and mechanical properties of RDX-CMDB propellant,the compatibility of HCCT with the main components of RDX-CMDB propellant was tested and the performances of three kinds of RDX-CMDB propellants with different contents of HCCT were measured by target line method,methyl violet test,adiabatic method,etc.The results show that HCCT has good compatibility with the main components NC+NG and RDX of RDX-CMDB propellant,the addition of HCCT makes the burning rate of the propellant at the pressure of 2-6MPa decrease and the burning rate pressure exponent increase,the heat of detonation,fraction sensitivity and impact sensitivity all decrease,the tensile strength and elongation rate remain basically unchanged,and it has no effect on the chemical stability of the propellant." @default.
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- W2750664401 date "2016-01-01" @default.
- W2750664401 modified "2023-09-23" @default.
- W2750664401 title "Effects of Hexachlorocyclotriphosphazene on Performance of RDX-CMDB Propellant" @default.
- W2750664401 hasPublicationYear "2016" @default.
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