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The aim of this paper is to provide an overview of the main physico-chemical and ballistic characteristics of modern solid rocket propellants.In this regard, oxidizers, metallic fuels, and various additives are presented and their role is discussed.Furthermore, the experimental methods and the mathematical models used to determine the ballistic parameters (pressure, thrust, burning rate and specific impulse) are detailed.For a better understanding and exemplification, the burning process and static tests of on a subscale rocket motor are presented, the tests being performed using an environmentally friendly propellant developed in the Military Technical Academy "Ferdinand I".
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Dîrloman et al. (2023) studied this question.
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