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 nec...

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Bibliographic Details
Published in:Russian journal of physical chemistry. B 2021-07, Vol.15 (4), p.611-621
Main Authors: Zyuzin, I. N., Gudkova, I. Yu, Lempert, D. B.
Format: Article
Language:English
Subjects:
Chemistry
Chemistry and Materials Science
Combustion
Combustion temperature
Enthalpy
Explosion
Metal fuels
Physical Chemistry
Rocket propellants
Shock Waves
Solid rocket propellants
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Summary: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.
ISSN:1990-7931
1990-7923
DOI:10.1134/S1990793121040138