Abstract
The energy capabilities of solid composite propellants based on certain derivatives of 1,2,4- and 1,3,4-oxadiazoles, have been recently described in the literature on the assumption that they could be used as energy compounds, have been studied. It was shown that some of the compounds under investigation have a good potential for creating solid propellants with improved energy characteristics. The quantitative dependences of the energy parameters of the propellant on the properties of the oxidizer under study, aluminum content in the formulation, of the type of binder and of its fraction are established.
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Funding
The work was completed in the Institute of Problems of Chemical Physics, RAS (research issue no. 0089-2014-0019 “Elaboration of high-energy materials and technologies for the developed and perspective systems”), supported by the Presidium of the Russian Academy of Sciences “Elaboration of solid propellants and fuels for the gas generators of the athodyds of hypersonic aircraft and study of the heat mass exchange and combustion in gas generators” in terms of Program 56, “Fundamental bases of the breakthrough technologies for national security.”
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Gudkova, I.Y., Zyuzin, I.N. & Lempert, D.B. The Energy Capabilities of New Derivatives of 1,2,4- and 1,3,4-Oxadiazoles as Components of Solid Composite Propellants. Russ. J. Phys. Chem. B 14, 302–313 (2020). https://doi.org/10.1134/S1990793120020062
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DOI: https://doi.org/10.1134/S1990793120020062