REPUBLIC OF SERBIA MINISTRY OF DEFENCE
MINISTRY OF DEFENCE Material Resources Sector Defensive Technologies Department
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Composite SOLID PROPELLANTS with octogene
VESNA RODIĆ Military Technical Institute, Belgrade, springvesna63@gmail.com MARICA BOGOSAVLJEVIĆ Military Technical Institute, Belgrade, marica.radusinovic@gmail.com ALEKSANDAR MILOJKOVIĆ Military Technical Institute, Belgrade, zabackermit@gmail.com SAŠA BRZIĆ Military Technical Institute, Belgrade, sasabrzic@gmail.com
Abstract: Composite solid propellants based on ammonium perchlorate/hydroxyterminated polybutadiene/isophorone dyisocyanate including different contents of octogene (HMX) have been represented in this paper. The mass of HMX increased in relation to oxidant, with constant bimodal fraction ratio. Combustion of the propellants has been improved by adding of titanium (IV) oxide powder as stabilizer. Parameters of burning rate laws and apparent viscosity values were determined and compared for the propellants of the same total solid phase. Key words: Composite solid propellant, octogen, titanium (IV) oxide, ballistic bahaviour.
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