Abstract
In the two-phase flow of a solid propellant rocket motor, condensed combustion products suffer a set of physical and chemical transformations, which constitute the condensed combustion products evolution process. The process of condensed combustion products formation in the surface layer of burning propellants and their evolution in the gas phase determines efficiency of the metal fuel as a component of solid rocket propellant. The objective of this paper is the experimental study of the evolution of condensed combustion products in the gas phase of burning solid rocket propellants.
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