Abstract
Heat release kinetics in the reaction of thermal decomposition of 7-amino-7H-difurazano[3,4-b:3′4′-f] furoxano[3″,4″-d]azepine and a binary rocket propellant on its basis, suggested as a potential promising dispersing agent in the gas generator of propulsive jet engines. The fundamental kinetic aspects found in the study were used to calculate the time in which a certain degree of decomposition is reached at a prescribed set of temperature for solving the problem of applicability of the propellant under consideration for a particular article.
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Funding
The study was financed by the Institute of Problems of Chemical Physics, Russian Academy of Sciences: research topics 0089-2019-0005 “Basic and problem-oriented research in the field of development of condensed energetic systems for various purposes” (State registration number AAAA-A19-119100800130-0) and 0089-2019-0017 “Integrated basic and problem-oriented studies in the field of physics and chemistry of combustion and heat and mass exchange in high energy solid and liquid propellants (combustibles) and new generation materials for high temperature combustion chambers of propulsive jet engines.”
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Russian Text © The Author(s), 2019, published in Zhurnal Prikladnoi Khimii, 2019, Vol. 92, No. 13, pp. 1657–1665.
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Kazakov, A.I., Lempert, D.B., Nabatova, A.V. et al. Kinetic Fundamental Aspects of Heat Release in Thermal Decomposition of 7-Amino-7H-difurazano[3,4-b:3′4′-f] furoxano[3″4″-d]azepine and Binary Fuel on Its Basis. Russ J Appl Chem 92, 1696–1704 (2019). https://doi.org/10.1134/S1070427219120101
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DOI: https://doi.org/10.1134/S1070427219120101