In this articlethe the possibility of application of detonation nanodiamond (DND) as a prospective component of composite solid propellants (CSP) and additive approach to opti-mization of fuel compositions based on binary fuel compositions is considered. The introduc-tion to the fuel composition of DND allows creating a metal-free CSP with increased energy-to-mass characteristics. Usage of the additive approach for calculations when creating new prospective compositions of CSP allows reducing significantly the volume of work to optimize the fuel compositions and to simplify the process of thermodynamic engineering.

Key words: nanodiamond, solid rocket fuel, components, compositions, energy-mass and ballis-tic characteristics

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2016, Т. 59, № 8, Стр. 96-100


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