INVESTIGA TION OF WA YS TO CONTROL THE LEVEL OF GAS-DYNAMIC LOADS DURING THE LA UNCH OF A SPA CE ROCKET
The article describes the possibilities of controlling the level of gas dynamic loads during the launch of a space rocket. The possibilities of a software package developed with the participation of the authors for the study of gas dynamic loads on the elements of the gas flue during the launch of a space rocket, taking into account changes in the parameters of the gas reflector together with the operation of the cooling system of the launch device, are briefly described. Modeling with the help of the developed software package allows us to obtain estimates of the influence of the angle of inclination or the length of individual sections of the gas reflector on the pressure and temperature values acting on the structure. The picture of the interaction of the water jet of the cooling system with the jet of the propulsion system is reflected.