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

Heat release kinetics in the reaction of thermal decomposition of 7-amino-7 H -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.