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2017, vol. 67, br. 1, str. 3-12
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Preliminarna istraživanja kompozitnih raketnih goriva sa oktogenom
Preliminary research of composite rocket propellants including octogene
Sažetak
U radu su prikazana istraživanja kompozitnih raketnih goriva na bazi amonijum perhlorata, hidroksiterminiranog polibutadiena i izoforon diizocijanata sa različitim udelima oktogena (HMX). Masa HMX je povećavana na račun oksidatora, konstantnog bimodalnog sastava. Sagorevanje goriva je stabilizovano dodatkom titanijum (IV) oksida. Određivani su parametri zakona brzine sagorevanja i poređeni sa vrednostima za goriva istih sastava čvrstih faza. Takođe su određivane vrednosti prividnog viskoziteta, jednoosnih mehaničkih karakteristika, gustina i energetskih vrednosti istih sastava.
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 were determined and compared for the propellants of the same total solid phase. Also, the apparent viscosity, uniaxial mechanical characteristic, density and energetic values were determined for the same formulations.
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