Abstract
We studied the effect of modifier additives TiB2, AlMgB14, (NH4)2TiF6, NH4BF4, Ca3(PO4)2 on the combustion parameters of composite propellants based on aluminum powder as a fuel (about 20% wt.), ammonium perchlorate as an oxidizer (about 60% wt.), and energetic binder (MPVT about 20% wt.). As a result of the study, the influence of additives on the rate of composite propellants combustion, dimensionless mass and agglomerate size was revealed.
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