VERIFICATION OF MODEL OF CALCULATION OF INTRA-CHAMBER PARAMETERS IN HYBRID SOLID-PROPELLANT ROCKET ENGINES

摘要

On the basis of obtained analytical estimate of characteristics of hybrid solid-propellant rocket engine verification of earlier developed physical and mathematical model of processes in a hybrid solid-propellant rocket engine for quasi-steady-state flow regime was performed. Comparative analysis of calculated and analytical data indicated satisfactory comparability of simulation results.