A computer-aided approach for primary optimization of propellant formu
lations is described. The computer code includes a database containing
information of approximately 1000 propellant components and 1600 comb
ustion products. Possible ways of designing the advanced components of
composite solid propellants (binders, plasticizers, curative agents,
and oxidizers) are considered. The physicomechanical and physicochemic
al behavior (and related phenomena) of material with a high content of
disperse components, determined by theology and mechanical and kineti
c parameters, is analyzed in detail.