“…Combustion products of high-energy rocket propellants are multi-component mixtures with high stagnation temperatures. The presence of condensed particles in the combustion products leads to the formation of a two-phase flow, which develops under conditions of transition from the continuum flow regime to the rarefied flow regime [4,5]. Particles of the condensed phase not only affect the functioning of space technology, being deposited, for example, on the elements of optical systems, but are also long-lived formations, creating a special form of pollution of the space environment [6][7][8].…”