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Two phase analysis of solid rocket motor plume as particle characteristics  

Kim, Seong-Lyong (열공력팀)
Kim, In-Sun (열공력팀)
Publication Information
Aerospace Engineering and Technology / v.9, no.1, 2010 , pp. 17-27 More about this Journal
Abstract
KSLV-I KM plume including alumina particle has been studied using the continuum solver. Alumina particles are assumed to have 7 different diameters, and the specific ratio of the plume gas is assumed to be 1.2, with which the internal nozzle flow characteristics are similar to those of the chemically equilibrium analysis results. The results showed that the expansion angle of the particles is smaller than that of the gas phase, and that the big sized alumina particles are gathered in the plume core and the expansion angles of the big sized particles are smaller than those of the light particles. When the emissivity of the particles are assumed to be 0.1, the radiative heat flux is equivalent to those measured during the flight test of KSLV-I.
Keywords
KSLV-I; Kick Motor; solid rocket motor; plume; plume radiatinv heating;
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