Energy Abilities of Certain Derivatives of 1,2,4,5-Tetrazine N-Oxides as Components of Solid Composite Rocket Propellants

The energy capabilities of five real-life high-enthalpy derivatives of 1,2,4,5-tetrazine N-oxides as components composite solid rocket propellants (CSRPs), which do not contain metallic fuel, are considered. Various ways of reducing the combustion temperature of CSRPs to an acceptable value, if necessary, are studied.